Year of Launch 2013RAE Table of Earth Satellites Page 1Name Cospar ID Launchdate Shape and Size Date of Orbital Nodal Semi Perigee Apogee Orbital Argument
[Launcher] [Norad#] + Launch site Lifetime + Descent dateweight (kg)(m)orbitalInclinationperiodmajor axisheightheighteccentricityof perigee
FragmentCospar ID[Norad#]Descent dateLifetimedetermination(deg)(min)(km)(km)(km)(deg)
Cosmos 2482 *2013 01 A2013 Jan 15.6832013 Jan 15.7482.50115.737867147515030.002288
[Rokot / Breeze-KM][39057]2252013 Jan 16.0782.49115.757868147615020.002283
PLE-LC133/3
Cosmos 2483 *2013 01 B2013 Jan 15.6832013 Jan 15.9982.50115.757868147815010.002278
[39058]225
Cosmos 2484 *2013 01 C2013 Jan 15.6832013 Jan 15.9982.50115.807870148015030.001292
[39059]225
Breeze-KM2013 01 D2013 Jan 15.683Cylinder2.6 long2013 Jan 15.9982.49115.887874148715040.001306
Upperstage[39060]122002.5 dia
IGS 8A #2013 02 A2013 Jan 27.194No TLE issued. Orbits from amateur observations.
[H-2A][39061]2016 Aug 1.9897.4694.8868915115140.000279
TAN
IGS 8B ##2013 02 B2013 Jan 27.194No TLE issued. Orbits from amateur observations.
[39062]2016 Aug 1.9997.1493.1068054254290.000333
DH-2A 2nd stage2013 02 C2013 Jan 27.194Cone+Cyl9.2 longNo TLE issued
[39063]738 days31004 dia
2015 Feb 4
Fragments2013 02 D-G4 pieces, 1 has decayedFor orbital information see extra pages at end of year
STSAT-2C $2013 03 A2013 Jan 30.2922013 Jan 30.3480.2993.02728029215110.084166
[KSLV-1][39068]100
NARO
KSLV-1 2nd stage2013 03 B2013 Jan 30.292Cylinder2013 Jan 30.4880.2793.08728329615130.084165
[39069]
*Strela-3M (Rodnik-S) satellites.
#4th Radar Information Gathering Satellite. ## Optical demonstration satellite.
$1st orbital launch by South Korea.
TDRS-11 (K)2013 04 A2013 Jan 31.075Box +2 panels7.92 high2013 Jan 31.3425.73713.18264424336357910.595180
[Atlas-5][39070]> million years+2 dishes2013 Feb 4.9416.08855.332984811155357850.413181
CC-LC413454 full21 span2013 Feb 5.5710.041089.073506421588357840.202183
1769 dry4.57 dia2013 Feb 7.087.551353.684053632529357860.040184
2013 Feb 9.517.061426.924198535424357880.004176
2013 Feb 11.567.011436.124216535780357940.0002263
DAtlas-5 2nd stage2013 04 B2013 Jan 31.075Cylinder12.68 long2013 Jan 31.3326.07686.68257834145346630.592179
(Centaur)[39071]2100?3.05 dia
Globalstar M0782013 05 A2013 Feb 6.670Trapezoidal0.60 x 1.502013 Feb 6.7352.00103.4272999139270.001194
[Soyuz 2-1a/Fregat][39072]box + 2 panelsx 1.602013 Feb 6.8052.01103.4773019189260.0006227
BAI-LC31/6700 full12 span
350 dry
Globalstar M0932013 05 B2013 Feb 6.670Trapezoidal0.60 x 1.502013 Feb 6.8752.01103.4873029199270.0005222
[39073]box + 2 panelsx 1.602013 Feb 7.3052.01103.4373009169260.0007238
700 full12 span
350 dry
Globalstar M0942013 05 C2013 Feb 6.670Trapezoidal0.60 x 1.502013 Feb 2.8752.01103.4773019199270.0005227
[39074]box + 2 panelsx 1.602013 Feb 7.0252.01103.4372999159260.0007241
700 full12 span
350 dry
Globalstar M0952013 05 D2013 Feb 6.670Trapezoidal0.60 x 1.502013 Feb 6.8752.01103.4773019189260.0006227
[39075]box + 2 panelsx 1.602013 Feb 7.3052.01103.4372999159260.0008234
700 full12 span
350 dry
Globalstar M0962013 05 E2013 Feb 6.670Trapezoidal0.60 x 1.502013 Feb 6.8752.05103.5273039189310.0009321
[39076]box + 2 panelsx 1.602012 Feb 7.0252.01103.4773019199260.0005228
700 full12 span
350 dry
Globalstar M0972013 05 F2013 Feb 6.670Trapezoidal0.60 x 1.502013 Feb 6.8752.01103.4372999159260.0007244
[39077]box + 2 panelsx 1.602013 Feb 10.1852.01103.4773019199260.0005240
700 full12 span
350 dry
Fregat stage201305 G2013 Feb 6.670Spheres +1.5 highDe-orbited on 1st orbit??
[NNA]nozzle3.3 dia
1100?
Amazonas 32013 06 A2013 Feb 97.900Box + 2 panels8.1 x 2.92013 Feb 7.696.34632.7824416247358270.729181
[Ariane-5 ECA][39078]> million years6265x 3.62013 Feb 9.012.03730.90268785293357060.567185
KOU-ELA326 span2013 Feb 10.331.79909.883110413753356980.353180
2013 Feb 12.650.571213.823769326938356910.116182
2013 Feb 13.790.151398.834143234411356960.016188
2013 Feb 14.660.101429.974204535628357040.009236
2013 Feb 15.560.091434.534213435697358140.00115
2013 Feb 28.390.071436.104216535776357960.000237
Azerspace 12013 06 B2013 Feb 97.900Box +2 panels5.6 x 2.52013 Feb 7.706.04632.3524404261357900.728178
[39079]> million years3275x 3.22013 Feb 10.113.23741.48271375750357670.553180
?? span2013 Feb 13.780.831348.324042931510365900.063213
2013 Feb 19.980.051436.104216535777357960.00028
Ariane-5 2nd stage201306 C2013 Feb 97.900Drum-cone3.5 long2013 Feb 7.716.04631.2724376260357360.728178
[39080]28803.94 dia
Sylda 5A upperpart201306 D2013 Feb 97.900Barrel shaped 6.4 long2013 Feb 8.526.04632.1524399262357790.728178
[39081]517 4.6 dia
DProgress-M 18M &2013 07 A2013 Feb 11.612Cyl+beehive+7.5 long2013 Feb 11.6051.6588.5865831792290.00465
[Soyuz-U][39082]165 days+spheroid+2.72 maxdia2013 Feb 11.7051.6390.2366642752960.002283
BAI-LC1/52013 Jul 262 panels2.3 dia2013 Feb 11.7451.6592.7567884014170.001263
7250?
DSoyuz-U 3rd stage2013 07 B2013 Feb 11.612Cylinder8.1 long2013 Feb 11.6051.6588.6265851842280.00369
[39083]2.272 days2400?2.66 dia2013 Feb 13.8151.6287.2265151321400.000799
2013 Feb 13.884 ^
Landsat 8 *2013 08 A2013 Feb 11.751Box + panel2013 Feb 11.7998.2598.2570546676840.001300
[Atlas-5 401][39084]27819 span2013 Feb 11.8698.2598.2770556686840.001293
(AV-035)VDB-LC3E
Atlas-5 2nd stage #2013 08 B2013 Feb 11.751Cylinder12.68 long2013 Feb 11.7998.2498.4070616796860.0005217
(Centaur)[39085]heliocentric2100?3.05 dia2013 Feb 11.8698.2798.4370626347330.00762
Progress-M 18M docked 2013 Feb 11.858 with ISS (Pirs port). Undocked 2013 Jul 25.863
^Decay observed over north western Europe (Belgium, Netherlands, Germany)
*Landsat Data Continuity Mission
#After satellite deployment the remaining fuel was used to send the stage to a heliocentric disposal orbit. Decayed administrately 2013 Feb 12.
SARAL *12013 09 A2013 Feb 25.522Box +2 panels2013 Feb 25.5698.6499.5771167057700.00553
[PSLV C-20)][39086]4092013 Feb 25.7798.6599.5871177067720.00550
SRI-LC12013 Feb 27.7398.63100.4571597727880.001251
2013 Mar 2.5298.52100.4571587767840.0006249
AAUSAT 3 *42013 09 B2013 Feb 25.522Cube0.10 side2013 Feb 25.7798.63100.4371587727870.001269
[39087]3
Sapphire *22013 09 C2013 Feb 25.522Cube1.0 side?2013 Feb 25.7798.63100.4571597747860.0008269
[39088]1482013 Feb 25.9198.63100.4371577727860.001268
NEOSSat *32013 09 D2013 Feb 25.522Box2013 Feb 25.7798.63100.4571587767840.0006284
[39089]742013 Feb 25.9198.63100.4271577727850.0009275
2013 Feb 26.9698.63100.4271577717860.001264
STRaND-1 *72013 09 E2013 Feb 25.522Box +2 panels0.30 x 0.102013 Feb 25.7798.62100.3871557717820.0008295
[39090]6.5x 0.10
2x 0.30x0.10
BRITE *52013 09 F2013 Feb 25.522Cube0.10 side2013 Feb 25.7798.64100.3771557697830.001324
[39091]14
UniBRITE *62013 09 G2013 Feb 25.522Cube0.10 side2013 Feb 25.7798.63100.4571597727880.001264
[39092]14
PSLV 4th stage2013 09 H2013 Feb 25.522Cylinder2.0 long2013 Feb 9898.62100.4271577727840.0008296
[39093]2.8 dia2013 Feb 28.9598.6599.5871177067710.00540
Fragment (DLA U)#2013 09 J[39094]Bowl2013 Feb 25.9898.61100.3871557707830.0009271
*1 Satellite with Argos and ALtika from India/France; *2 Space Surveillance satellite from Canada; *3 Near-Earth Object Surveillance Satellite from Canada;
*4 Aalborg University Satellite from Danmark; *5 aka TUGSat 1 (Technical University Graz)from Austria; *6 BRIght-star Target Explorer from Austria,
Canada and Poland; *7 Surrey Training, Research and Nanosatellite Demonstrator from Great Brittan
#Dual Launch Adapter Upperpart
DDragon CRS2 &2013 10 A2013 Mar 1.632Blunt cone4.4 high2013 Mar 1.7151.6789.7766412053190.00946
[Falcon 9][39115]25.058 days+ cylinder3.66 dia2013 Mar 1.8251.6889.7566412033220.00950
CC-LC402013 Mar 26.690+ 2 panels + cylinder2.8 high 2013 Mar 1.9651.6791.0867063143400.002 320
575 cargo+ 2 panels16.5 span2013 Mar 2.0351.6891.7867413214040.006 12
2013 Mar 2.0851.6792.5067763914030.0008212
2013 Mar 2.4751.7292.9767983325070.013129
2013 Mar 2.7265.6893.3768184334450.0009329
2013 Mar 3.4351.6592.7567884014170.001335
2013 Mar 26.4751.6592.4367723794080.002163
DFalcon 9 2nd stage2013 10 B2013 Mar 1.632Cylinder10.1 long2013 Mar 1.7751.6689.7366402053180.00846
[39116]9.496 days3.66 dia
2013 Mar 11.128 %
DFragments *2013 10 C[39117]2013 Mar 43 days2013 Mar 1.7151.6889.6766371973190.00944
2013 Mar 4.1751.6787.6865391471740.00274
2013 10 D[39118]2013 Mar 43 days2013 Mar 1.7151.6689.6266342003120.00849
2013 Mar 3.8551.6787.7865431511780.00260
SBIRS GEO-22013-11 A2013 Mar 19.890Box+ 2 panels2013 Mar 1922.1918535786#
[Atlas 5-401][39120]> million years~4500
(AV-037)(USA241)CC-LC41
Atlas-5 2nd stage2013 11 B2013 Mar 19.890Cylinder12.68 longIn Geo Transfer Orbit
(Centaur)[39121]2100?3.05 dia
CRS2 is the second re-supply flight to the ISS. After launch 3 of the 4 thrusterpods were not activated automatically and the solar panels not deployed.
They were activated by a command override and the solar panels deployed. Rendez-vous with ISS delayed till 2013 Mar 3 and grappled 2013 Mar 3.438 by the
stations robotic arm. Berthed 2013 Mar 3.580 to ISS (Harmony nadir port) by ground control from Houston and Canada. CRS2 was early 2013 Mar 26 unberthed
from the ISS by the robotic arm and released 2013 Mar 26.455
*Fragments are the solar array covers.
%Decayed at 46°S, 111° W
#No TLE released, orbit from pre-launch information.
Satmex 82013 12 A2013 Mar 26.796Box +2 panels2013 Mar 26.851.5173173^
[Proton-M/Breeze-M][39122]> million years54732013 Mar 26.8650.32705000^
(#384)BAI-LC200/392013 Mar 26.9549.142535800^
2013 Mar 27.1718.38615935786^
2013 Mar 27.4318.38750.20273486118358230.5430
2013 Mar 28.5110.41870.683020411826358260.3970
2013 Mar 29.774.831103.223536720973370040.2270
2013 Mar 31.760.271391.334128434004358070.0221
2013 Apr 1.660.181405.834157034582358010.015349
2013 Apr 1.900.051435.924216135767357980.0004178
2013 Apr 5.700.041436.084216535777357950.0002182
Breeze-M stage201312 B2013 Mar 26.796Stubby Cyl2.62 long2013 Mar 27.1718.38615935786^
[39123]1220~2.4 dia2013 Mar 27.4818.12760.90261385392341260.5505
Breeze-M tank201312 C2013 Mar 26.796Torus2.1 long2013 Mar 26.9549.48321.6715551330180160.569354
[39124]12904.1 dia
0.8 cross
DSoyuz-TMA 08M $2013 13 A2013 Mar 28.863Cyl+beehive+7.5 long2013 Mar 28.8651.6589.2366152132600.004192
3M[Soyuz-FG][39125]166.261days+spheroid+2.72 maxdia2013 Mar 29.0651.6592.7767884014180.00183
RBAI-LC1/52013 Sep 11.1242 panels2.3 dia
7250?
DSoyuz-FG 3rd stage2013 13 B2013 Mar 28.863Cylinder8.1 long2013 Mar 28.8651.6788.6865881972210.00254
(Blok I)[39126]3 days2400?2.66 dia2013 Mar 31.0651.6587.2265151281450.00147
2013 Mar 31
Anik G12013 14 A2013 April 15.817Box +2 panels2013 Apr 16.4313.91760.52276007950344910.4814
[Proton-M/Breeze-M][39127]> million years49052013 Apr 19.604.141096.083521521840358330.1991
(#385)BAI-LC200/392013 Apr 20.690.141411.054167334786358030.01231
2013 Apr 20.750.441415.374136434183357880.019359
2013 Apr 24.600.031434.924214235741357850.0005224
2013 Apr 25.350.011435.104214535749357840.0004138
2013 Apr 26.540.001436.154216635776357990.000398
2013 Apr 26.680.011436.104216535773358000.0003120
2013 14 continued on next page
^Orbits from pre-launch information.
$Soyuz-TMA 08M with 2 cosmonauts (Vinogradov and Misurkin) and 1 astronaut (Cassidy) was launched on a fast track and docked 2013 Mar 29.103 with ISS
(Poisk port)after a 5:45 hours flight. Undocked 2013 Sep 10.982 from ISS.
Breeze-M stage201314 B2013 April 15.817Stubby Cyl2.62 long2013 Apr 16.4313.40812.43288429104358220.4630
[39128]1220~2.4 dia
Breeze-M tank201314 C2013 April 15.817Torus2.1 long2013 Apr 15.9348.40378.9517347346215910.612356
[39129]12904.1 dia
0.8 cross
Fragment2013 14 D[43407]2018 Apr 17.0414.63751.90273917712343120.486358
Bion-M1 #2013 15 A2013 Apr 19.417Sphere +2013 Apr 19.5764.8892.6367822525540.02262
[Soyuz 2-1A][39130]Cylinder2013 Apr 21.9064.8969.0569485585800.002203
BAI-LC31/66800
DOSSI 1 *2013 15 B2013 Apr 19.417Cube0.10 side2013 Apr 21.5064.9492.6367822585490.02159
[39131]80 days0.952013 Jul 7.4264.8888.7265901772450.00527
2013 Jul 8
Dove 2 *2013 15 C2013 Apr 19.417Box0.30 x 0.102013 Apr 22.0364.8896.0769495595810.002199
[39132]5.5x 0.10
AIST 2 *2013 15 D2013 Apr 19.417Box2013 Apr 22.0364.8896.0569485585810.002205
[39133]53
Beesat 3 *2013 15 E2013 Apr 19.417Cube0.10 side2013 Apr 22.0364.8896.0069465545800.002211
[39134]1
SOMP *2013 15 F2013 Apr 19.417Cube0.10 side2013 Apr 22.0364.8896.0069465545800.002212
[39135]1
Beesat 2 *2013 15 G2013 Apr 19.417Cube0.10 side2013 Apr 22.0364.8896.0069465555790.002213
[39136]1
DSoyuz 2-1A2013 15 H2013 Apr 19.417Cylinder6.74 long2013 Apr 19.6264.9192.6067802525520.02261
3rd stage[39137]106 days44002.66 dia2013 Aug 2.9364.8787.5265301371660.002337
2013 Aug 3
#The descent capsule of Bion M landed in the region Orenburg, Russia.
*OSSI 1 (Open Source Satellite Initiative)from South Korea was released 2013 Apr 19.676 on orbit 4-6; Beesat (Berlin Experimental and Educational Satellite)2
and 3, SOMP (Student’s Oxygen Measurement Project) from Germany were released 2013 April 21 on orbit 30-33; Dove 2 from USA was released 2013 April 21 on
orbit 30-33; AIST 2 released 2013 April 21 on orbit 34-35.
DPhonesat v1b &2013 16 A2013 Apr 21.875Cube0.10 side2013 Apr 21.9451.6189.4566252362570.0025
(Bell)[39142]6 days1
[Antares 110]WLI-LC0A2013 Apr 27
DDove 1 $2013 16 B2013 Apr 21.8753U cube0.30 x 0.102013 Apr 22.0751.6089.4066242362550.001347
[39143]6 days6.0x 0.102013 Apr 26.7351.6287.7765431601680.0006316
2013 Apr 27
DPhonesat v2 &2013 16 C2013 Apr 21.875Cube0.10 side2013 Apr 24.7651.6288.9266002102320.002339
(Alexander)[39144]6 days12013 Apr 27.3451.6087.3365211331520.00140
2013 Apr 27
DAntares A-ONE #2013 16 D2013 Apr 21.875Cylinder2013 Apr 24.9051.6289.3566212342500.0010
[39145]19 days38002013 May 9.5051.6187.6065341521590.0005315
2013 May 10
DPhonesat v1a &2013 16 E2013 Apr 21.875Cube0.10 side2013 Apr 24.8351.6388.9065992132270.001345
(Graham)[39146]5 days12013 Apr 26.5551.6287.8365461611740.001234
2013 Apr 26
DAntares 2nd stage2013 16 F2013 Apr 21.875Cylinder3.5 long2013 Apr 24.8951.6089.2066142262440.001357
(Castor 30A)[39147]10 days12262.34 dia2013 May 1.8551.6287.4265251431490.0005266
2013 May 1
DProgress-M 19M %2013 17 A2013 Apr 24.425Cyl+beehive+7.5 long2013 Apr 24.7951.6491.0067022933530.004163
[Soyuz-U][39148]56 days+spheroid+2.72 maxdia2013 Apr 26.3751.6591.0367042973540.004165
BAI-LC1/52013 Jun 192 panels2.3 dia2013 Apr 26.7751.6592.7567884024160.001186
7250?2013 Jun 11.6351.6693.2868144164560.00356
2013 Jun 11.9551.6492.5567783924070.001272
2013 Jun 19.4651.6592.3367683594190.004336
DSoyuz-U 3rd stage2013 17 B2013 Apr 24.425Cylinder8.1 long2013 Apr 24.8551.6388.4765771842130.00287
[39149]2 days2400?2.66 dia2013 Apr 26.0151.6387.6765381541550.0009103
2013 Apr 26
#First test flight of the Antares rocket with a dummy payload, a 3800 kg aluminium block to simulate the Cygnus spacecraft.
The ID’s of the A and D object were interchanged after the objects already had decayed, based on the observation of the decay of the D object over Chile.
$Technoly demonstration nanosatellite. Deployed before the dummy mass was separated from the 2nd stage.
Named Phonesat for the use of a smart phone as board computer from NASA Ames research Center. Deployed before the dummy mass was separated from the 2nd stage.
%Progress-M 19M docked 2013 Apr 26.518 with ISS (Zvezda aft port); a KURS antenna did not deploy, but no problem with the automatic docking. Undocked
2013 Jun 11.582 and stayed in orbit for the Radar Progress Experiment.
2013 2018 – version 1.1218
Year of Launch 2013RAE Table of Earth Satellites Page 1Name Cospar ID Launchdate Shape and Size Date of Orbital Nodal Semi Perigee Apogee Orbital Argument
[Launcher] [Norad#] + Launch site Lifetime + Descent dateweight (kg)(m)orbitalInclinationperiodmajor axisheightheighteccentricityof perigee
FragmentCospar ID[Norad#]Descent dateLifetimedetermination(deg)(min)(km)(km)(km)(deg)
Gao Fen 1 *2013 18 A2013 Apr 26.1762013 Apr 26.2998.3797.7070276356620.002202
[CZ-2D][39150]2013 May 1.7898.0797.5570206286540.002224
(#Y18)JIUQ
NEE-01 Pegasus * #2013 18 B2013 Apr 26.176Box + 2 panels0.20 x 0.102013 Apr 26.2998.0697.5570206306530.002242
[39151]1.2x 0.10
0.64 span
Turksat 3USAT *2013 18 C2013 Apr 26.176Box0.30 x 0.102013 Apr 26.3698.0697.5870226336530.001247
[39152]x 0.10
CubeBug 1 * #2013 18 D2013 Apr 26.176Cube0.10 side2013 Apr 27.0398.0897.5370196286530.002243
[39153]2
CZ-2D 2nd stage2013 18 E2013 Apr 26.176Cilinder7.5 long2013 Apr 27.1098.0797.5370196296530.002247
[39154]40003.35 dia2013 May 1.8698.3697.7070276356630.002187
Cosmos 24852013 19 A2013 Apr 26.224Cyl+ 2 panels+2.4 dia2013 Apr 26.3464.94339.8016131249192550.589240
(Glonass M)[39155]1 million yearsmagnometerboom3.7 height2013 Apr 26.4764.74683.872571219169194990.00661
[Soyuz 2-1b/Fregat]PLE-LC43/413707.2 span2013 Apr 27.6864.73678.282582319223196670.009117 2013 May 1.07 64.77 676.90 25537 19139 19178 0.0008 291
Fregat stage201319 B2013 Apr 26.224Spheres +1.5 high2013 Apr 26.4764.74683.872571219169194990.00661
[39156]nozzle3.3 dia2013 Apr 28.1464.78676.552552919128191720.0009270
1100?
Chinasat 112013 20 A2013 May 1.671Box +2 panels2013 May 1.7726.74762.0027635183423310.763179
[CZ-3B][39157]> million years52342013 May 10.630.651436.234216735775358030.000344
XI2013 may 15.450.641436.074216435771358000.000363
CZ-3B 3rdstage2013 20 B2013 May 1.671Cylinder12.38 long2013 May 1.9626.64778.5328034225430860.764179
[39158]30603.0 dia
*Gao Fen (High Resolution) is a Chinese Earth resource satellite. NEE-01 Pegasus is the 1st Equadorian satellite. Turksat 3USAT is radio amateur satellite
from Turkey. CubeBug 1 is from Argentina.
#It was reported that both satellites were hit by debris from the Cosmos 1666 3rd stage, that past witin 1 km on 2013 May 23. Contact was lost with NEE-01
Pegasus and CubeBug 1 was spinning faster; both also had a small inclination change. The rocket 1985 58 B was launched 1985 Jul 8.
Proba-V *2013 21 A2013 May 7.088Box0.84 x 0.762013 May 7.1698.74101.0371867878280.003257
[Vega][39159]138.2x 0.732013 May 7.7298.73101.2071948118200.000654
(VV-02)KOU-ZLV
VNREDSat 1 #2013 21 B2013 May 7.088Cube + panel0.6 side2013 May 7.3198.1498.1770506696730.000348
[39160]115.31.2 span
ESTCube 1 %2013 21 C2013 May 7.088Cube0.10 side2013 May 7.5298.1398.0370436586700.0009231
[39161]1.3305
VESPA upperpart &2013 21 D2013 May 7.0882013 May 7.3098.7499.6771216708150.01058
[39162]
DVega 4th stage2013 212013 May 7.088Cylinder1.74 long
[NNA]7801.9 diaDe-orbited after release of 2013 21 B and C
Eutelsat 3D2013 22 A2013 May 14.668Box +2 panels2013 May 15.3017.57762.58276496782357600.5240
[Proton M/Breeze M][39163]> million years54782013 May 22.320.061330.404205335603357460.002262
(#386)BAI-LC200/392013 May 22.800.071332.754209935678357630.001153
2013 May 23.140.051433.574211535707357670.0007182
2013 May 24.590.031436.204216735783357930.000162
2013 Jun 8.980.021436.074216435784357870.00003245
Breeze-M stage201322 B2013 May 14.668Stubby Cyl2.62 long2013 May 15.3017.95712.20264185868342100.5364
[39164]1220~2.4 dia
Breeze-M tank201322 C2013 May 14.668Torus2.1 long2013 May 14.8249.51325.3215669336182440.571354
[39165]12904.1 dia2013 may 15.0549.53324.7815652336182110.571354
0.8 cross2013 may 15.7249.50325.1015662335182320.571355
*Project for On-Board Autonomy and Vegetation is a earth observing satellite from Belgium
#Vietnamese optical earth satellite
%Estonian cubesat
VEga Secondary Payload Adapter; a multiple satellite dispenser.
USA 242 (GPS 2F-4)2013 23 A2013 May 15.901Box +2 panels2.51 wide2013 May 16.1054.98729.802685120449204970.0009309
[Atlas 5-401][39166]1 million years15402.05 deep2013 May 16.9055.00729.102683420449204630.0003323
(AV-039)Navstar 68CC-LC412.25 high
Atlas-5 2nd stage2013 23 B2013 May 15.901Cylinder12.68 long5516720200^
(Centaur)[39167]2100?3.05 dia2013 May 16.1055.57767.902777820457223420.034295
2013 May 16.1655.38750.872736620452215220.020289
WGS 5 (USA 243)2013 24 A2013 May 25.019Box +2 panels2016 Jan 12.780.031436.124216535774357990.000321 *
[Delta 4 M+ 5,4][39168]> million years598840.84 span
CC-LC37B
Delta 4 2nd stage2013 24 B2013 May 25.019Cylinder12.00 long25.30184.86874.6^
[39169]28502.44 dia24440.866853.5^
DSoyuz-TMA 09M $2013 25 A2013 May 28.855Cyl+beehive+7.5 long2013 May 28.9151.6588.7065891942270.00368
3M[Soyuz-FG][39170]166.262 days+spheroid+2.72 maxdia2013 May 29.1251.6592.8767934084210.00110
RBAI-LC1/52013 Nov 11.1172 panels2.3 dia
7250?
DSoyuz-FG 3rd stage2013 25 B2013 May 28.855Cylinder8.1 long2013 May 28.8551.6588.7765921922340.00376
(Blok I)[39171] days2400?2.66 dia
SES 62013 26 A2013 Jun 3.388Box +2 panels2013 Jun 4.5426.341380.63410724484649030.736180
[Proton M/Breeze M][39172]> million years61102013 Jun 13.110.111435.854216035678358850.002286
(#387)BAI-LC200/392013 Jun 13.730.111436.604217535693359000.002301
2013 Jun 14.130.111437.524219335753358750.001287
2013 Jun 14.760.131437.724219735743358930.002290
2013 Jun 15.090.121437.754219735745358930.002289
2013 Jun 17.250.111436.084216535756358150.0007303
Breeze-M stage201326 B2013 Jun 3.388Stubby Cyl2.62 long2013 Jul 1.6727.851303.00395182941633370.764186
[39173]1220~2.4 dia
Breeze-M tank201326 C2013 Jun 3.388Torus2.1 long2013 Jun 3.6450.72276.1514048406149320.517172
[39174]12904.1 dia
0.8 cross
^Orbit from pre-launch press releases. * Orbit from amateur observations
$Soyuz-TMA 09M docked 2013 May 29.090 with ISS (Rassvet port) with Expedition 36 cosmonaut Yurchikhin, NASA astronaut Nyberg and ESA astronaut Parmitano.
On 2013 Nov 1.356 the Soyuz undocked from the Rassvet module and was relocated to the Zveda aft port in a 21 minute flight. Undocked 2013 Nov 10.976 from ISS.
ATV 4 *2013 27 A2013 Jun 5.911Cylinder10.27 long2013 Jun 5.9851.6289.7066382522660.001278
’Albert Einstein’[39175]+ 4 panels4.48 dia2013 Jun 10.9651.6590.4066732883010.00185
[Ariane 5ES]KOU-ELA32006022.32 span2013 Jun 12.7951.6590.5066772923050.00163
9778 dry2013 Jun 14.8651.6592.2867653753990.00288
2013 Jun 15.0651.6592.4867753894040.00153
2013 Jun 15.2651.6292.5767793924090.00143
2013 Jun 15.3251.7192.3267673793970.0014
2013 Jun 15.3351.6592.7067853984150.00152
2013 Jun 15.6251.6592.8567934074210.00173
DAriane 5 2nd stage2013 27 B2013 Jun 5.911Drum-cone3.5 long2013 Jun 5.9851.6289.5566312502540.0003335
[39176]< 1 day28803.94 dia
2013 Jun 6
Cosmos2486 #2013 28 A2013 Jun 7.765Cylinder2013 Jun 7.9098.3193.2768131866830.03679
[Soyuz 2-1b][39177]+ 2 panels
PLE-LC43/46500
Soyuz 2-1B2013 28 B2013 Jun 7.765Cylinder8.1 long2013 Jun 7.9098.3193.4868231877030.03879
3rd stage[39178]24002.66 dia
(Blok 1)
DShenzhou 10 %2013 29 A2013 Jun 11.401Cylindrical2.941 long2013 Jun 11.5742.7889.6066331983100.008130
3M[CZ-2F][39179]14.604 daysInstrument/2.5 dia2013 Jun 11.7142.7890.2566662603130.004138
RJIUQ2013 Jun 26.005propulsion +2.8 basedia2013 Jun 12.7842.7890.9566993153270.0009290
2 panels;17 span2013 Jun 13.5442.7891.2067123283380.0008295
Dome-shaped2.5 high2013 Jun 15.6942.7891.1867113273380.0008316
Descent mod;2.52basedia2013 Jun 25.4942.7891.2267133323370.0004135
Cylindrical2.8 long2013 Jun 25.5542.7891.2267133323370.0004134
Orbital mod2.25 dia
8500
DCZ-2F 3rd stage2013 29 B2013 Jun 11.401Cylinder~14.2 long2013 Jun 11.6542.6291.1767101894740.021121
[39180]10 days4950?3.35 dia2013 Jun 11.6542.7989.5866331973110.009132
2013 Jun 212013 Jun 21.6342.7787.2865181311490.001216
Shenzhou 10 &2013 29 H2013 Jun 11.401Cylindrical2.8 long2013 Jun 26.4942.7991.2367133323370.0004132
Orbital module[39193]Orbital mod2.25 dia
Fragments2013 29 C-G5 pieces, all in orbitFor orbital information see extra pages at end of year
*ATV 4 docked 2013 Jun 15.588 with ISS (Zvezda aft port) with about 7 tons of cargo.Undocked 2013 Oct 28.372 with 2163 kg of trash and disposed equipment.
#2nd Persona optical reconnaissance satellite with a 1.5 m dia mirror.
%Shenzhou 10 with 3 astronauts (Nie Haisheng, Zhang Xiaogang and Wang Yaping(2nd Chinese female astronaut))docked 2013 Jun 13.216 with Tiangong 1.
On 2013 Jun 23 Shenzhou 10 was undocked and redocked manually 2013 Jun 23.088. Finally undocked 2013 Jun 25
The module separated shortly before the de-orbit burn of Shenzhou 10.
Resurs P12013 30 A2013 Jun 25.728Cylinder2013 Jun 25.7997.2991.5567292464550.01658
[Soyuz 2-1b][39186]+ 2 panels2013 Jun 26.7097.2891.6067322494570.01555
BAI-LC31/665802013 Jun 29.1797.2893.8068394494710.002256
2013 Jun 29.2497.2893.8368414534720.001262
2013 Jun 29.8497.2893.9068444584720.001275
DSoyuz 3rd stage2013 30 B2013 Jun 25.728Cylinder8.1 long2013 Jun 25.8597.3091.6767352494630.01660
(Blok 1)[39187]92 days24002.66 dia2013 Sep 25.0897.2587.1865131291400.000851
2013 Sep 25
Fragment2013 30 C[39226]2013 Aug 2397.2893.89455474
O3B FM5 *2013 31 A2013 Jun 25.810Trapezoidal3.0x1.62013 Jun 25.860.04280.6314199780778340.001129
[Soyuz 2-1bST-B][39188]box + 2 panelsx ~1 high2013 Jun 26.430.04280.7014201780778380.001135
(VS-05)KOU-ELS7002013 Jul 7.030.04287.9314444806480670.0001341
O3B FM42013 31 B2013 Jun 25.810Trapezoidal3.0x1.62013 Jun 25.860.04280.8014205781878340.0006115
[39189]box + 2 panelsx ~1 high2013 Jun 26.440.03280.8814207781978380.0007135
7002013 Jul 7.230.04287.9314444806280690.000220
O3B FM22013 31 C2013 Jun 25.810Trapezoidal3.0x1.62013 Jun 25.860.05280.8814207781978380.0007141
[39190]box + 2 panelsx ~1 high2013 Jun 26.440.04281.0014212782878370.0003109
7002013 Jul 8.530.03287.9314444806280690.0002106
O3B PFM2013 31 D2013 Jun 25.810Trapezoidal3.0x1.62013 Jun 25.860.04281.2214219783978410.00008331
[39191]box + 2 panelsx ~1 high2013 Jun 27.810.03283.7214303784280060.006164
7002013 Jul 5.880.03287.9314444806280680.000287
Fregat stage $2013 31 E2013 Jun 25.810Spheres +1.5 high2013 Jun 25.860.07279.0014144769378380.005166
[39192]nozzle3.3 dia2013 Jun 26.050.09276.2714052765876880.001357
1100?
Cosmos 24872013 32 A2013 Jun 27.7452013 Jun 27.7674.9094.9268774535440.007223
(Kondor)[39194]
[Strela]BAI-LC175/591150
Strela 3rd stage2013 32 B2013 Jun 27.745Cylinder~1.2 long2013 Jun 27.8374.7494.5568764935010.0006291
[39195]2.5 dia
*Other 3 Billion; reffering to the 3 billion people with limited or no internet access.
$After satellite deployment the stage was put in a higher lower disposal orbit
IRIS #2013 33 A2013 Jun 28.103Cylinder3.17 long2013 Jun 28.1597.9197.5270186166630.003179
[L-1011/Pegasus XL][39197]+ 2 panels1.82 maxdia2013 Jun 28.2197.9197.5570206206630.003176
VDB5.45 span
Pegasus-XL 3rdstage2013 33 B2013 Jun 28.103Cylinder1.34 long2013 Jun 28.1597.9197.4870176206560.003173
(Orion 38)[39198]1200.97 dia
IRNSS-R1A *2013 34 A2013 Jul 1.758Cube +2 panels1.58x1.52013 Jul 1.8617.91360.9716793282205480.603179
[PSLV-XL (C22)][39199]1425x1.52013 Jul 8.4727.021430.504205535483358710.005179
SRI-LC1624 dry6 span2013 Jul 15.6127.021432.204208935497359230.005175
2013 Jul 16.0427.021434.934214235659358680.002181
2013 Jul 17.9127.031435.304214935686358550.002179
2013 Jul 18.9227.031436.134216635706358680.002185
2013 Jul 27.7827.041436.104216535703358700.002185
PSLV-XL 4th stage2013 34 B2013 Jul 1.578Cylinder2.6 long2013 Jul 1.6417.79306.8316975282209110.608179
[39200]2920 full2.02 dia
Shijan 11-052013 35 A2013 Jul 15.3942013 Jul 15.4498.1098.6070706807030.002210
[CZ-2C][39202]2013 Jul 15.5198.1198.6870746887040.001200
JIUQ-LC43/6032013 Jul 17.7798.1098.6870746887040.001206
CZ-2C 2nd stage2013 35 B2013 Jul 15.394Cilinder7.5 long2013 Jul 15.4598.1499.1270956847490.005275
[39203]40003.35 dia2013 Jul 15.5198.1499.0570926777490.005273
2013 Jul 17.5798.1499.0570926777490.005266
Fragments2013 35 C-F[39204]4 pieces, all in orbitFor orbital information see extra pages at end of year
MUOS-2 &2013 36 A2013 Jul 19.542Box +2 panels6.70x3.66No TLE issued
[Atlas-5 551)[39206]> million years+ 2 dishesx1.832013 Jul 19.66719.1380235787
(AV-040 )CC-LC41680027.50 span2013 Jul 21.39714.60786.00784735822%
5.39 + 14.0
Dia
Atlas-5 2nd stage2013 36 B2013 Jul 19.542Cylinder12.68 longNo TLE issued
(Centaur)[39207]2100?3.05 dia2013 Jul 21.39718.73685.89357535194%
#Interface Region ImagingSpectrograph is a sun observatory.
*Indian Regional Navigation Satellite System will be made up with 4 satellites in MEO and 3 satellites in GEO.
Mobile User Objective System
%Orbit from SSR
Shiyan Weixing-7Chuang Xin-32013 37 A2013 Jul 19.9842013 Jul 20.1198.0698.087045660673 0.0009 26
[CZ-4C][39208]
WUZ
Chuang Xin-3Shiyan Weixing-72013 37 B2013 Jul 19.9842013 Jul 20.1298.0698.137048666673 0.0005 56
[39209]
Shijan-152013 37 C2013 Jul 19.9842013 Jul 20.1298.0698.1270476646730.000640
[39210]
CZ-4C 3rd stage2013 37 D2013 Jul 19.984Cylinder4.93 long2013 Jul 20.1198.1096.1569534786710.01444
[39211]17462.90 dia
Fragments2013 37 E-J5 pieces, all in orbitFor orbital information see extra pages at end of year
Alphasat2013 38 A2013 Jul 25.829Box +2 panels7.1 x 2.52013 Jul 25.613.45632.3324404224358270.729177
[Ariane 5 ECA][39215]> million years+ dishx 2.82013 Jul 27.382.51684.62257322879358270.640179
(V214)KOU-ELA3665040 span2013 Jul 27.901.19847.472966510751358220.423178
2013 Jul 29.710.121265.603875828731360270.094303
2013 Aug 1.300.021434.424213235702358050.001346
2013 Aug 1.800.021434.504213335703358060.001350
2013 Aug 6.240.021436.534217335782358090.0003345
2013 Aug 10.290.021436.374217035775358090.0004214
2013 Aug 12.250.021436.084216435786357860.0000116
Insat-3D2013 38 B2013 Jul 25.829Box + panel2.4x1.62013 Jul 25.633.41630.9224368200357780.730177
[39216]> million years2120x1.52013 Jul 26.513.45632.9324420231358510.729178
2013 Jul 31.740.271428.284201235469357970.00410
2013 Aug 2.710.261430.734206035567357950.00311
2013 Aug 6.610.241434.334213035720357830.000833
2013 Aug 7.800.251435.874216035749358150.000834
2013 Aug 12.730.241436.084216535781357910.0001226
Ariane-5 2nd stage2013 38 C2013 Jul 25.829Drum-cone3.5 long2013 Jul 25.623.47633.2224427223358740.730178
[39217]28803.94 dia
Sylda 5A upperpart2013 38 DC2013 Jul 25.829Barrel shaped 6.4 long2013 Jul 25.623.47633.2224427223358740.7301782013 Jul 25.64 3.33 634.18 24452 227 35918 0.730 173
[3921839219]517 4.6 dia
Ariane-5 2nd stage2013 38 D2013 Jul 25.829Drum-cone3.5 long2013 Jul 25.643.33634.1824452227359180.730173
[39218]28803.94 dia
DProgress-M 20M %2013 39 A2013 Jul 27.865Cyl+beehive+7.5 longNo TLE issued. Used 4-orbit fast ascent
[Soyuz-U][39219]199 days+spheroid+2.72 maxdia2014 Feb 3.7751.6792.8867944124180.0005103
BAI-LC1/52014 Feb 112 panels2.3 dia2014 Feb 4.0051.6892.4867753724210.004268
7250?2014 Feb 11.4451.6592.3067663614130.004231
DSoyuz-U 3rd stage2013 39 B2013 Jul 27.865Cylinder8.1 long2013 Jul 27.9251.6488.5765821892180.00265
[39220]3 days2400?2.66 dia2013 Jul 30.0651.6287.1765121271400.001141
2013 Jul 30
DKounotori 4 *2013 40 A2013 Aug 3.825Cylinder10.06 long2013 Aug 3.9351.6589.3866221873010.009313
(HTV-4)[39221]35 days158764.27 dia2013 Aug 4.3851.6490.3566702813020.002288
[H-2B]TAN2013 Sep 712020 empty 2013 Aug 7.5751.6592.8867944134180.0004284
2013 Aug 8.1551.6492.3267673793970.001192
2013 Aug 9.0551.6592.6367824024040.0002251
2013 Aug 9.1151.6492.7267863904250.003191
2013 Aug 9.1851.6192.8267914064190.001162
2013 Aug 9.3851.6592.8867944134180.0004291
2013 Aug 10.7151.6592.8867944134180.0004298
2013 Sep 7.1351.6590.1066581514080.019300
DH-2B 2nd stage2013 40 B2013 Aug 3.825Cone+Cyl10.6 longDeorbited within 1 orbit before being catalogued.
[NNA]< 0.18 day3000?4 dia
2013 Aug 3
WGS-62013 41 A2013 Aug 8.020Box +2 panels2013 Aug 825.61856852#
(USA 244)[39222]> million years598840.84 span2013 Aug 82443966894#
[Delta 4M+5,4]CC-LC37
Delta 4 2nd stage2013 41 B2013 Aug 8.020Cylinder12.00 longNo TLE issued
[39223]28502.44 dia
Kompsat 52013 42 A2013 Aug 22.610Octagonal2013 Aug 22.6697.6095.4869215335520.001290
[Dnepr][39227]cylinder2013 Aug 23.1597.6095.5269225355520.001302
YAS-LC370/13+2 panels
+radar panel
1402
Dnepr 3rd stage2013 42 B2013 Aug 22.610Cylinder2013 Aug 23.4497.50102.47725454112100.046184
[39228]3.05 dia
DFragment2013 42 C[39229]2015 Oct 9778 days2013 Aug 22.6697.6095.2369085115480.003334
2015 Oct 9.8597.5287.5765331471610.001253
%Progress-M 20M docked 2013 Jul 28.101 with ISS (PIRS port). Undocked 2014 Feb 3.681 and will stay in orbit for 8 days for the Izgib experiment.
*HTV 4 rendez-vouzed 2013 Aug 9 with ISS and was grappled 2013 Aug 9.478 by the station’s robotic arm and berthed 2013 Aug 9.651 to the Harmony Node
nadir port. HTV 4 was unberthed 2013 Sep 4.505 and was released from the stations arm 2013 Sep 4.683
#Orbits from press releases.
USA 245 (NROL-65)*2013 43 A2013 Aug 28.752Stubby Cyl2013 Aug 28.8197.9497.2370042639890.052212
[Delta 4 Heavy][39232]2013 Aug 28.8697.8897.2570052579970.053193
(#7)VDB-SLC62013 Aug 30.8897.8897.32700925710040.053186
2015 Mar 30.9197.9297.67702626910250.054271
2016 Aug 1.8797.8997.3270092649970.052318
Delta 4 2nd stage 2013 43 2013 Aug 28.752Cylinder13.7 longDe-orbited over Pacific Ocean at the end of the 1st orbit.
[NNA]0.063 day33505.1 dia
2013 Aug 28.815
Eutelsat 25B %2013 44 A2013 Aug 29.854Box + 2 panels7.2 x 2.22013 Aug 29.903.46629.7024336238356770.728178
[Ariane 5 ECA][39233]> million years6310x 2.32013 Sep 2.210.74965.333235516197357560.302177
(V570)KOU-ELA325.5 span2013 Sep 4.120.081434.024212435725357660.000519
2013 Sep 6.650.081434.304213035734357680.000438
2013 Sep 6.780.081434.757213835747357720.0003104
2013 Sep 7.100.081434.884214135750357750.0003125
2013 Sep 8.090.071436.234216735787357900.0000490
2013 Sep 9.850.071436.084216535784357880.00005189
GSAT-72013 44 B2013 Aug 29.854Box + 2 panels3.1 x 1.72013 Aug 29.913.40637.3024532288360180.728177
[39234]> million years2650x 2.02013 Aug 31.310.38979.933268116805357990.291164
~ 8 span?2013 Sep 3.930.221428.384201435471357990.00428
2013 Sep 6.130.221429.054202735526357710.00313
2013 Sep 7.960.221433.984212435680358100.00224
2013 Sep 11.910.211433.624211635675358010.00114
2013 Sep 15.500.201436.084216535758358140.0007336
Ariane-5 2nd stage2013 44 C2013 Aug 29.854Drum-cone3.5 long2013 Aug 29.913.59633.3324430253358490.729182
[39235]28803.94 dia
Sylda 5A upperpart2013 44 D2013 Aug 29.854Barrel shaped 6.4 long2013 Aug 29.913.49639.9224599303361370.728179
[39236]517 4.6 dia
AMOS 42013 45 A2013 Aug 31.837Box +2 panels2013 Sep 1.3926.88684.57257302861358420.6410
[Zenit 3 SLB][39237]> million years35002013 Sep 1.4926.85811.37288174175407010.6340
BAI-LC45/12013 Sep 6.660.661350.504047232388358000.042356
2013 Sep 9.940.051331.234207035577358050.003288
2013 Sep 13.760.051330.824206235576357900.003279
2013 Sep 17.030.061432.054208635625357890.002272
2013 Sep 19.890.051436.154216635784357910.00008132
2013 Sep 26.600.051436.124216535773358000.0003110
Zenit 3 SLB 3rd2013 45 B2013 Aug 31.837Cylinder4.5 long2013 Sep 5.1526.86683.55257052859357930.6411
Stage (Blok DM-SLB)[39238]18003.7 dia
*Possible a Keyhole satellite. No TLE’s issued. Orbits from amateur observations.
%Part of the payload was payed for by Qatar and is named Es’hail 1
Yaogan 17 A2013 46 A2013 Sep 1.8032013 Sep 1.9563.41107.127471107611100.00236
[CZ-4C][39239]2013 Sep 4.6363.41107.177474107611150.00342
JIUQ-LC6032013 Sep 5.8963.41107.257478108311160.00240
Yaogan 17 B2013 46 B2013 Sep 1.8032013 Sep 1.9563.41107.107471107611080.00235
[39240]2013 Sep 2.1063.41107.137472107611110.00238
2013 Sep 6.6463.41107.277479108411160.00244
Yaogan 17 C2013 46 C2013 Sep 1.8032013 Sep 1.9563.41107.127472107911080.00234
[39241]2013 Sep 2.1063.41107.157474107911100.00238
2013 Sep 6.6363.41106.577446105510800.002341
CZ-4C 3rd stage2013 46 D2013 Sep 1.803Cylinder4.93 long2013 Sep 1.8563.46105.05737589011040.01524
[39242]17462.90 dia2013 Sep 2.0963.47105.13737989011110.01524
Fragment2013 46 E[39243]2013 Sep 1.9563.41107.157473107811110.00242
2013 46 F[39244]2013 Sep 1.9563.41107.127471107711080.00236
2013 Sep 2.1063.41107.137473107711110.00237
2013 Sep 3.9663.41106.777456105910970.0039
2013 Sep 4.9263.41106.657450105810850.0020
2013 Sep 6.5563.41106.577446105510800.002341
2013 Sep 6.6463.41107.157474107911110.00237
DLADEE *2013 47 A2013 Sep 7.144Stubby hexa-2.37 long2013 Sep 737.6200278000
[Minotaur 5][39246]233.1 daysgonal cyl1.85 wide2013 Sep 13.7236.0111284.7516665620273185280.950155
WLI-LC0B2014 Apr 28.23831.85 deep2013 Sep 21.49511520
2013 Oct 1.4138.6014283.0719500314533757960.960157 Moon orbit insertion 2013 Oct 6.456 1388.4 538 15020 0.76
2013 Oct 9.4432402902220
2013 Oct 13.148235250
2013 Oct 20113<5050-100
DMinotaur 5 4thstage2013 47 B2013 Sep 7.144Cylinder2.076 long2013 Sep 737.4294.1205745
(Star 48V)[39248]50 days1551.245 dia2013 Nov 13.8537.4090.9767001894540.02012
2013 Nov 272013 Nov 26.6337.3988.1365601522120.005130
Minotaur 5 5thstage2013 472013 Sep 7.144Cylinder1.690 longIn similar orbit as first 2013 47 A orbit
(Star 37FM(V))[NNA]820.935 dia
*Lunar Atmosphere and Dust Environment Explorer launched in a highly elliptical orbit was captured2013 Oct 6 after 3.5 orbits by the moon’s gravity.
On 2013 Oct 6 it used the onboard motor to break into Lunar orbit. Ladee crashed 2014 Apr 28 between 04:30 and 05:22 UT on the far side of the Moon some
800 m from the rim of the Sundman V crater. The impact point was identified on a photo by the Lunar Reconnaissance Orbiter.
Cosmos 2488 *2013 48 A2013 Sep 11.9742013 Sep 12.0382.47116.027880149415100.001343
Gonets-M 05[Rokot/Breeze KM][39249]280
[Rokot/Breeze KM]PLE-LC133/3
Cosmos 2489 *2013 48 B2013 Sep 11.9742013 Sep 12.2282.49115.987879149315070.0009323
Gonets-M 06[39250]280
Cosmos 2490 *2013 48 C2013 Sep 11.9742013 Sep 12.2282.50116.007879149515070.0008331
Gonets-M 07[39251]280
Breeze KM2013 48 D2013 Sep 11.9742013 Sep 12.0482.48112.437717117515020.021272
Upperstage[39252]2013 Sep 12.2882.49112.507720117915040.021269
SPRINT-A #2013 49 A2013 Sep 14.208Box +2 panels2013 Sep 14.2729.77102.9072748059860.01238
(Hisaki)[39253]3482013 Sep 14.3429.75102.7872698079740.01136
[Epsilon]KAG2013 Sep 14.4829.75102.8072698089730.01137
Epsilon 4th stage2013 49 C2013 Sep 14.2082013 Sep 14.6429.72106.28743395211560.01467
[39255]200
Fragment2013 49 B[39254]2013 Sep 14.2729.70104.70735984711140.018118
AEHF-3 (USA 246)2013 50 A2013 Sep 18.174Box +2 panels2013 Sep 1820.59927.8621750052
[Atlas 5-531][39256]> million years6170
(AV-040)CC-LC4127.13 span
DAtlas 5 2nd stage2013 50 B2013 Sep 18.174Cylinder12.68 long2013 Sep 1820.26888.4615048321
(Centaur)[39257]508.485 daysdays2100?3.05 dia
2015 Feb 8.659
*Gonets-M data reley satellite
#Spectroscopic Planet Observatory for Recognition of Interaction of Atmosphere. First flight of the Epsilon rocket.
DCygnus (Orb-D1)%2013 51 A2013 Sep 18.457Cylinder2013 Sep 18.6751.6489.8366452592730.001167
[Antares-110][39258]35.306 days+ 2 panels2013 Sep 18.7551.6589.9066482622770.001144
WLI-LC0A2013 Oct 23.7634100 full2013 Sep 18.9451.6391.1067072743840.008273
2013 Sep 19.3151.6391.8367433403880.004306
2013 Sep 20.1451.6292.4367733864020.001120
2013 Sep 20.2751.6392.5867803874150.002101
2013 Sep 20.9251.5992.8867954084240.001124
2013 Sep 21.2451.6592.7767894064150.000763
2013 Sep 21.7051.6392.8267914074180.000872
2013 Sep 21.7651.6592.8067904064170.000862
2013 Sep 23.3051.6593.0568034114370.00255
2013 Sep 23.4951.6392.9367974144220.0006114
2013 Sep 23.5551.6592.9567974174210.000385
2013 Sep 27.2951.6592.7067853994140.00122
2013 Sep 28.4751.6592.7767894084130.000482
2013 Sep 28.5951.6592.7867904094130.0003108
2013 Oct 22.6851.6392.8367914094170.0006117
2013 Oct 22.8851.6292.8267914104140.0003336
2013 Oct 23.2051.6492.9067954144190.0004109
2013 Oct 23.5351.6592.8067904104130.000252
DAntares 2nd stage2013 51 B2013 Sep 18.457Cylinder3.5 long2013 Sep 18.6951.6189.8566452612730.0009152
(Castor 30A)[39259]21 days12242.36 dia2013 Oct 9.6051.6487.2365161331410.000737
2013 Oct 9
FengYun 3C2013 52 A2013 Sep 23.130Box + panel2013 Sep 23.1898.81101.0571878018150.001204
[CZ-4C][39260]22032013 Sep 23.4698.81101.0771888048150.0008218
WUZ2013 Sep 26.7698.81101.1371918088170.0006181
2013 Sep 27.2098.80101.2071948068240.001159
2013 Sep 27.6398.81101.2871988178220.0004173
2013 Sep 28.6898.82101.4072038218290.000536
CZ-4C 3rd stage2013 52 B2013 Sep 23.130Cylinder4.93 long2013 Sep 23.2698.84100.5071607588060.00345
[39261]1730?2.9 dia
Fragments2013 52 C-F4 pieces; all in orbitFor orbital information see extra pages at end of year
DKuaizhou 1 #2013 53 A2013 Sep 25.1932013 Sep 25.4296.6690.2066632752930.001280
[Kuaizhou][39262]706 days2013 Sep 27.4596.6690.4266732853040.001180
JIUQ2015 Sep 12013 Sep 27.7196.6590.5766812993050.0005234
2013 Oct 16.8496.6690.1866622792880.0007185
2013 Oct 17.2396.6590.5266782883120.002312
2013 Nov 1.1796.6690.1566602692950.002255
2013 53 A continued on next page2013 Nov 1.4396.6690.6066822903170.002 3
%Cygnus aborted the approach to ISS 2013 Sep 22.229 due to faulty GPS readings. A second attempt was made 2013 Sep 29. At Sep 29.458 the station’s robotic
Arm captured Cygnus and berthed it 2013 Sep 29.530 to the earth facing port of the Harmony module. Cygnus was unberthed by the stations robotic arm and
released 2013 Oct 22.480
#First launch of the quick response orbital vehicle. Kuaizhou means Quick Vessel. The 4th stage remained attached to the satellite.
Kuaizhou-1 performed small orbit raisings once every 2 weeks to mantain
Its low orbit. In 2014 Sep the satellite started to move to a higher
orbit, probably because the fuel ran low.
2014 Sep 16.0896.5890.0066532592900.002224
2014 Sep 16.2696.5790.5566802873150.002347
2014 Sep 26.1396.5890.3266692753060.002297
2014 Sep 26.2696.5790.8766963003340.003179
2014 Sep 29.2396.5891.3867213333520.001316
2014 Oct 9.2696.5891.7567393413800.003166
2014 Oct 16.2196.5892.0367533733750.0002209
2014 Oct 30.2796.5792.2267623723940.002302
2015 Sep 1.1596.4886.9365011131310.001257
DSoyuz-TMA 10M $2013 54 A2013 Sep 25.874Cyl+beehive+7.5 long2013 sep 25.9051.6788.6865881952240.00268
3M[Soyuz-FG][39263]166.268 days+spheroid+2.72 maxdia2013 Sep 26.0051.6990.8766952983350.003222
RBAI-LC1/52014 Mar 11.1422 panels2.3 dia2013 Sep 26.0751.6592.8767934134170.000385
7250?
Soyuz-FG 3rd stage2013 54 B2013 Sep 25.874Cylinder8.1 long2013 Sep 25.8751.6888.5865831912170.00242
(Blok I)[39264] days2400?2.66 dia
Cassiope *2013 55 A2013 Sep 29.667Hexagonal1.80 dia2013 Sep 29.7480.96100.87717926113390.075146
[Falcon 9 v1.1][39265]box1.25 high2013 Oct 7.5281.00103.10728432514860.080137
VDB-SLC4E481
CU-Sat 1 &2013 55 B2013 Sep 29.6672013 Sep 29.7380.99102.88727330614830.081160
[39266]54.552013 Sep 30.2981.02103.08728332014890.080157
Dande #2013 55 C2013 Sep 29.667Sphere2013 Sep 29.7481.00102.43725227714700.082156
[39267]50 full2013 Oct 7.4580.99103.10728432514850.080137
38 dry
POPACS 1 %2013 55 D2013 Sep 29.667Sphere0.10 dia2013 Sep 29.7480.99103.38729740314330.071156
[39268]2013 Oct 7.5281.00103.00727932414760.079137
2013 55 continued on next page
$Soyuz-TMA 10M with 2 cosmonauts (Kotov and Ryazanskiy) and an astronaut (Hopkins) docked 2013 Sep 26.031 with ISS (Poisk port). Undocked 2014 Mar 10.001
*CAScade Smallsat and IOnospheric Polar Explorer has a combined payload for communications test and observation of solar storms in the ionosphere.