Year of Launch 2015RAE Table of Earth Satellites(Issued 2015)Page 1

Year of Launch 2015RAE Table of Earth Satellites(Issued 2015)Page 1

NameCospar IDLaunch dateShape andSizeDate of OrbitalNodalSemiPerigeeApogeeOrbitalArgument

[Launcher] [Norad#] LaunchsiteLifetime and descent dateweight (kg)(m)orbitalInclinationperiodmajor axisheightheighteccentricityof perigee

FragmentCospar ID[Norad#]Descent dateLifetimedetermination(deg)(min)(km)(km)(km)(deg)

DDragon CRS-5 #2015 01 A2015 Jan 10.408Blunt cone4.4 high2015 Jan 10.4151.6490.0866572063510.01147

R[Falcon 9v1.1][40370]31.623 days+ cylinder3.66 dia2015 Jan 10.8151.6789.9866522063420.01047

CC-LC402015 Feb 11.031+ 2 panels2.8 high 2015 Jan 11.1251.7889.8866481933450.01154

8700 full16.5 span2015 Jan 11.3651.6591.5267283453530.0005275

2317 cargo2015 Jan 11.8251.6692.4867753834090.00225

2015 Jan 12.3851.6592.7067864034110.0006243

DFalcon 9 2nd stage $201501D B %2015 Jan 10.408Cylinder~14 long2015 Jan 10.4151.6590.126659205356 0.011 472015 Jan 10.54 51.66 89.90 6648 199 339 0.011 50

[4037340371]7 3 days49003.66 dia2015 Jan 12.8351.6288.2265651622100.004 502015 Jan 17.71 51.64 87.62 6535 141 172 0.002 76

2015 Jan 1713

DFragments (Solar201501 B C D% 2 pieces, both have decayedFor orbital info see extra pages at the end of the year

Panel covers)

MUOS 32015 02 A2015 Jan 21.045Box +2 panels6.7 x 3.66No TLE issued; in geostationary orbit. Orbits from amateur observations.

[Atlas-5 551][40374]> million years+ 2 dishesx 1.832016 Aug 1.104.481436.124216535554360190.006176

CC-LC 416740~30 span

5.4 + 14 dia

Atlas-5 2nd stage2015 02 B2015 Jan 21.045Cylinder12.68 long2015 Jan 20.8318.97704.68262323890358160.609179

(Centaur #223)[40375]22433.05 dia2015 Jan 21.5619.00688.95258403729351930.609178

#Dragon CRS-5 rendezvoused with ISS and was grappled 2015 Jan 12.454 by the stations robotic arm and 2015 Jan 12.579 berthed to the Harmony module (nadir port).Unbearthed 2015 Feb 10.708 and released 2015 Feb 10.799 from the robotic arm. Landed in the Pacific Ocean about 430 km SW of Long Beach, CA.

$Decay observed in Amur Region, Russia.

%Space-Track has object B as the r/b. Based on the re-entry dates object D is most likely the r/b and B, C the Solar panel covers.

SMAP #2015 03 A2015 Jan 31.599Pentagonal box1.5 x 0.92015 Jan 31.7298.1398.2070516606850.002215

[Delta II 7320-10C][40376]+spin platformx0.9

(#153)VDB-SLC-2W+ panel9.7 span

+ dish6.8 dia

944

Firebird 3 $2015 03 B2015 Jan 31.5991.5U Cube0.15 x 0.102015 Jan 31.8099.1395.7269324386690.017339

[40377]2x 0.10

Firebird 4 $2015 03 C2015 Jan 31.5991.5U Cube0.15 x 0.102015 Jan 31.8099.1395.7369324386690.017339

[40378]2x 0.10

Grifex ^2015 03 D2015 Jan 31.5993U Cube0.30 x 0.102015 Jan 31.8199.1395.7369334396690.017340

[40379]x 0.10

ExoCube (CP-10)2015 03 E2015 Jan 31.5993U Cube0.30 x 0.102015 Jan 31.8199.1295.7369324373700.017340

[40380]x 0.10

+ 2 booms0.25 long

DDelta II 2nd stage %2015 03 F2015 Jan 31.599Cylinder5.97 longDe-orbited

(Delta-K)[NNA]9502.44 dia

IGS 9 *2015 04 A2015 Feb 1.056No TLE issued. Orbits from amateur observations.

[H-IIA 202][40381]2016 Aug 1.9097.3594.2568614814840.000280

(F21)TAN-YOS-LC1

H-IIA 2nd stage2015 04 B2015 Feb 1.056Cylinder9.2 longNo TLE issued

[40382]4 dia

H-IIA 2nd stage2015 04 C[40383]No TLE issued

Fragment

#Soil Moisure Active/Passive; a NASA Environmental Research Satellite.

$Focused Investigations of Relativistic Electron, Intensity, Range and Dynamics. The satellites will study Space Weather.

^GEO-CAPE (GEOstationary Coastal and Air Pollution Events)ROIC (Read-Out Integrated Circuit)In-Flight performance Experiment.

From the California Polytechnic State University.

%The Delta-II 2nd stage lowered its orbit before deploying the cubsats; then made a de-orbit burn

*Information Gathering Satellite with a radar payload. Orbits based on amateur observations.

Inmarsat 5-F22015 05 A2015 Feb 1.522Box +2 panels6.98 high2015 Feb 2.1526.791377.20410044366648850.738180

[Proton-M/Breeze-M][40384]> million years+ antennas3.59 width2015 Feb 6.626.861762.734833818899650190.477180

BAI61003.27 long2015 Feb 8.142.012068.325377429915648760.325180

3750 bol33.80 span2015 Feb 12.600.211490.234321931892417890.114205

2015 Feb 18.340.121436.224216731550400270.101217

2015 Feb 23.850.131434.684213732436390810.079222

2015 Mar 3.620.101435.704215733261382960.060213

2015 Mar 5.480.091436.034216433274382960.060214

Breeze-M stage2015 05 B2015 Feb 1.522Stubby Cyl2.62 long2015 Feb 2.6528.071297.30394022816632320.767182

[40385]1220~2.4 dia

Breeze-M tank2015 05 C2015 Feb 1.522Torus2.1 long2015 Feb 2.4750.77274.2813984365148460.518172

[40386]12904.1 dia

0.8 cross

DFajr (Dawn)2015 06 A2015 Feb 2.368*Hexagonal Cyl2015 Feb 2.4155.5491.4767252234700.019162

[Safir][40387]24 days~502015 Feb 26.0355.5187.3765231341550.002231

SEM2015 Feb 26

Safir 2nd stage2015 06 B2015 Feb 2.368*Cylindrical~5 long2015 Feb 10.1955.5490.9266982194200.015182

[40388]1.25 dia

DIXV **2015 Sub2015 Feb 11.570Cone 5 long2015 Feb 115.476416

[NNA}0.070 days18452.2 wide

KOU-ZLV2015 Feb 11.6401.5 high

DIXV Avum **2015 Sub2015 Feb 11.570Cone-cyl2 long2015 Feb 115.476416

Upperstage[NNA]2.18 dia

[Vega] (#VV 04)

*Launch occurred around 08:50 UT according to outsiders.

**The Intermediate eXperimental Vehicle, a test space plane, was launched on a sub-orbital flight by the Vega rocket with the Attitude Vernier Upper Module. At a height of 332 km the IXV separates from the AVUM. IXV continues upwards to a maximum altitude of 412 km and then drops back to earth. The lifting body and parachutes slows the IXV down for a landing in the Pacific Ocean after a 100 min flight.

After spacecraft separation the AVUM made a short burn to raise the perigee to an altitude preventing a re-entry. At T+1:50 the AVUM made a de-orbit burn and probably burned up in the atmosphere over the Atlantic Ocean.

DSCOVR #2015 07 A2015 Feb 11.961Octagonal bus1.37 x 1.872015 Feb 11.96335185185

[Falcon 9 v1.1][40390]indefinitely+ Cylinder2015 Feb 11.98237.091871371148

CC-LC40+ panel +boom~7.5 span2015 Jun 8Entered orbit around L1 Lagrange point

750

~600 dry

Falcon 9 2nd stage 2015 07 B2015 Feb 11.961Cylinder~14 longInitial orbits similar to 2015 07 A

[40391]49003.66 dia2015 Feb 23.983Collision avoidance manoeuvre

2015 Apr 2.0059.26 37d148.354700203831075441760.171252

DProgress M-26M *2015 08 A2015 Feb 17.458Cyl+beehive+7.5 long2015 Feb 17.4851.6588.7265901862370.00491

[Soyuz-U][40392]178.137 days+spheroid+2.72 maxdia

BAI-LC1/52015 Aug 14.5952 panels2.3 dia

7287

DSoyuz-U 3rd stage2015 08 B2015 Feb 17.458Cylinder8.1 long2015 Feb 17.4851.6288.5765821862200.00373

[40393]2 days2400?2.66 dia2015 Feb 1951.6387.70153186

2015 Feb 19

Cosmos 2503 $2015 09 A2015 Feb 27.459Cylindrical4.0 x 2.32015 Feb 27.5397.6493.2568123275390.01672

(Bars-M 1L)[40420]4000x 2.3

[Soyuz 2-1A]PLE-LC43/4

DSoyuz 2-1A 3rd stage2015 09 B2015 Feb 27.459Cylinder6.74 long2015 Feb 27.6097.6493.2268103275360.01572

[40421]368.456 days23552.66 dia

2016 Mar 1.915

ABS 3A %2015 10 A2015 Mar 2.160Box +2 panels4.6 high2015 Mar 2.9724.821263.2738300391634520.823171

{Falcon 9 v1.1][40424]> million years+ 4 dishes2.1 wide2015 Mar 4.4524.811259.2238217358633190.824171

CC-LC4019542015 Mar 9.0924.981242.2838280434633690.822173

2015 Mar 11.3224.991246.5338368449635290.882173

2015 Apr 16.5012.431369.32408474272646650.739179

2015 Apr 23.0010.641387.15412015242644030.718180

2015 Apr 27.8810.001389.57412495731640100.706180

2015 May 8.007.881408.83416307579629220.665182

2015 May 12.017.161415.62417638261625070.649182

2015 May 21.835.881426.934198510280609330.603183

2015-10 continued on next page

#Deep Space Climate Observatory to measure space weather from the L1 Lagrange point at 1.5 million km on the Earth-Sun line.

*Progress M-26M docked 2015 Feb 17.706 with ISS (Zvezda port) with 2370 kg of supplies. Undocked 2015 Aug 14.430 for destructive re-entry over the south

Pacific Ocean.

$Cartographic satellite.

%First double payload launch of Falcon 9. Both satellites used their ion thrusters to achieve the geostationary orbit.

Eutelsat 115 West B2015 10 B2015 Mar 2.160Box +2 panels4.6 high2015 Mar 2.9724.981259.8238230359633430.824171

%[40425]> million years+ 4 dishes2.1 wide2015 Mar 4.324.811260.7238248360633790.824171

22052015 Mar 11.2824.991242.2338279439633630.822173

2015 Mar 17.3423.591243.97383151784620880.787174

2015 Mar 19.0722.681244.83383332005619030.781174

2015 Apr 20.5012.991348.48404323778643290.749181

2015 Apr 23.3312.251354.07405444123642070.741182

2015 Apr 30.8310.981361.75406974870637660.724183

2015 May 4.6710.021370.35408685382635960.712184

2015 May 12.018.641379.60410526634627120.683185

2015 May 17.047.671387.70412127342623250.667185

2015 May 21.836.891398.88414338151619580.649187

Falcon 9 2nd stage2015 10 C2015 Mar 2.160Cylinder~14 long2015 Mar 2.7624.941254.2238115363631080.823171

[40426]49003.66 dia2015 Mar 3.2324.951255.1238133364631450.823171

2015 Mar 4.4424.971255.5738142365631620.823171

MMS 1 #2015 11 A2015 Mar 1213.114Octagonal3.5 dia2015 Mar 13.1628.831409.3041639545699750.83419

[Atlas V-421][40482]cylinder1.23 high2015 Mar 13.3128.861413.7341726556701390.83419

(#53)CC-LC41+4 wire booms 60 long

+2 axial booms15 long

+2 rigid booms

1360

MMS 22015 11 B2015 Mar 1213.114Octagonal3.5 dia2015 Mar 13.1628.741407.3041599524699180.83419

[40483]cylinder1.23 high2015 Mar 13.3228.851414.1041733551701570.083419

+4 wire booms 60 long

+2 axial booms15 long

+2 rigid booms

1360

MMS 32015 11 C2015 Mar 1213.114Octagonal3.5 dia2015 Mar 13.1628.891412.0241692545700820.83419

[40484]cylinder1.23 high2015 Mar 13.6028.841414.6741744551701800.83419

+4 wire booms 60 long

+2 axial booms15 long

+2 rigid booms

1360

%First double payload launch of Falcon 9. Both satellites used their ion thrusters to achieve the geostationary orbit.

#Magnetospheric Multiscale Spacecraft to study the Earth’s magnetic field in a thetrahedron shaped formation. At first some 90 km apart, then closing

in to about 9 km.

MMS 42015 11 D2015 Mar 1213.114Octagonal3.5 dia2015 Mar 13.1628.961411.7241686540700760.83419

[40485]cylinder1.23 high2015 Mar 13.3328.821415.1341754552701980.83419

+4 wire booms 60 long

+2 axial booms15 long

+2 rigid booms

1360

Atlas-5 2nd stage2015 11 BE2015 Mar 1213.114Cylinder12.68 long2015 Mar 13.1628.841415.0041751556701890.83419

[40486]22433.05 dia

Ekspress AM-72015 12 A2015 Mar 18.920Box +2 panels7.5 high2015 Mar 19.6119.91734.13269585406357520.5630

[Proton-M/Breeze-M][40505]> million years5712 full30 span2015 Mar 20.8416.66766.05277336971357390.5190

BAI-LC200/391438.5 dry2015 Apr 7.780.021436.154216635780357940.0002107

2015 Apr 8.120.021436.124216535780357930.000297

Breeze-M stage2015 12 B2015 Mar 18.920Stubby Cyl2.62 long2015 Mar 19.5520.02682.38256754415341780.5805

[40506]1220~2.4 dia

Breeze-M tank2015 12 C2015 Mar 18.920Torus2.1 long2015 Mar 20.7549.47302.0314912333167340.550354

[40507]12904.1 dia

0.8 cross

GPS IIF-9 2015 13 A2015 Mar 25.775Box +2 panels2.49x2.032015 Mar 25.9555.02729.622684720463204730.0002194

(SVN 71) (USA 260)[40534]1 million years1630x2.242015 Mar 28.5955.01729.572684620466204680.00003235

[Delta 4M+4,2]CC-LC37B2015 Apr 2.6555.02726.532677120317204680.003229

2015 Apr 16.8855.02718.232656720182201940.000296

2015 Apr 20.6855.02717.922655920177201840.0001330

Delta 4 2nd stage2015 13 B2015 Mar 25.775Cylinder12.2 long2015 Mar 26.3454.69746.222725220788209590.003340

[40535]4 dia

Fragments2015 13 C-EF3 4 pieces all in orbitFor orbital info see extra pages at the end of the year

KOMPSAT-3A2015 14 A2015 Mar 25.923Hexagonal box3.5 long2015 Mar 25.9897.5195.3269125265400.001288

[Dnepr][40536]+ Cylinder2.0 dia2015 Mar 27.5697.5195.2569095215400.001277

DOM-LC370/13+ 3 panels~7 span

~1000

Dnepr 3rd stage2015 14 C2015 Mar 25.923Cylinder1.0 long2015 Mar 26.7097.38104.73736052314400.062185

[40541]23603.0 dia

Fragment2015 14 B[40537]2015 Mar 25.9897.5094.9768964995350.003331

IGS 102015 15 A2015 Mar 26.056No TLE issued, orbits from amateur observations.

(Optical 5)[40538]2016 Aug 1.9397.4894.8868915105150.0003350

[H-IIA 202]TAN-LC1

H-IIA 2nd stage2015 15 B2015 Mar 26.056Cylinder9.2 longNo TLE issued, orbits from amateur observations.

[40539]4 dia2016 Aug 1.9197.4693.9068434574720.001168

??Fragment2015 15 C[40540]

DSoyuz TMA-16M $2015 16 A2015 Mar 27.822Cyl+beehive+7.48 long2015 Mar 27.8151.6188.6065841982130.00154

3M[Soyuz-FG][40542]168.214 days+spheroid+2.72 maxdia

RBAI-LC1/52015 Sep 12.0362 panels2.2 dia

712010.6 span

Soyuz-FG 3rd stage %201516 B2015 Mar 27.822Cylinder6.74 long2015 Mar 28.0051.6188.9065992112300.001342

(Blok I)[40543]days24102.66 dia2015 Mar 28.2451.6188.4265751882040.00142

$Soyuz TMA-16M with 2 cosmonauts (Padalka and Kornienko) and an astronaut (Kelly) docked 2015 Mar 28.065with ISS.

Kornienkao and Kelly will stay aboard ISS for almost a year. They returned to earth 2016 Mar 2 aboard Soyuz TMA-18M (2015 43A)

On 2015 Aug 28 Soyuz TMA-16M was relocated to the Zvezda aft port with a 25 min free flight in order to free the Poisk port for Soyuz TMA-18M.

Soyuz TMA-16M undocked 2015 Sep 11 with Padalka, Mogensen and Aimbetov and landed 157 km SE of Dzhezkazgan.
Galileo 7 (263)2015 17 A2015 Mar 27.907Box +2 panels2.5 x 1.22015 Mar 28.1054.82835.872939422447235830.01996

(Adam)[40544]1 million years732.8x 1.12015 Mar 28.5555.06860.222996223563236040.0007248

[Soyuz2-1BST-B/Fregat]KOU-ELSZLS14.67 span2015 Mar 28.8655.07860.302996423562236080.0008 242

(VS11)2015 May 5.9255.15844.732960123217232280.0002262

Galileo 8 (264)2015 17 B2015 Mar 27.907Box +2 panels2.5 x 1.22015 Mar 28.1155.09859.922995523593235590.0006231

(Anastasia)[40545]1 million years732.8x 1.12015 Mar 28.6155.07859.502994523564235690.00009230

14.67 span2015 Mar 28.8655.06859.622994823566235720.0000988

2015 May 5.8355.14844.632959923213232270.0002271

Fregat MT2015 17 C2015 Mar 27.907Spheres1.5 long2015 Mar 28.1055.07860.032995823560235980.0006219

Upperstage[40546]+ nozzle3.35 dia

1050

IRNSS-1D2015 18 A2015 Mar 28.493Box +2 panels1.58x1.502015 Mar 28.6219.22301.2016801278205670.604178

[PSLV](C27)[40547]> million years1425 fullx1.502015 Mar 29.9419.22628.9824318310355690.725180

SRI603 dry~5 span2015 Apr 7.6530.481435.084214535699358340.002181

2015 Apr 9.6330.471436.004216335698358710.002183

2015 May 5.8630.431436.134216635697358760.002183

PSLV 4th stage2015 18 B2015 Mar 28.493Cylinder3.0 long2015 Mar 25.6519.08306.5316966277208970.608179

[40548]1.34 dia

Beidou-I1 S2015 19 A2015 Mar 30.576Box +2 panels2015 Apr 2.3454.981461.834266735796367810.012172

[CZ-3C/E - YZ-1][40549]2015 Apr 28.0954.981438.254220735662359950.004190

XI-LC22015 Apr 28.9254.951437.574219435760358700.001150

2015 May 9.0754.961435.804215935598359620.004175

DYuanZheng-1 stage *CZ-3C 3e stage2015 19 B2015 Mar 30.5762015 Mar 30.9654.93438.8219129194 25307 0.656 168

[40550]359 days2016 Mar 23.4954.5489.256616863890.022310

2016 Mar 23

YuanZheng-1 stage *2015 19 C2015 Mar 30.576

[41929]

*First launch with this new upper stage capable of up to 8 engine burns.

Gonets-3M No 212015 20 A2015 Mar 31.575Cylinder +2015 Mar 31.7382.49116.037881149715080.0007335

[Rokot/Breeze-KM][40552]booms

PLE-LC133/3282

Gonets-3M No 222015 20 B2015 Mar 31.575Cylinder +2015 Mar 31.7382.48116.027880149515070.0007324

[40553]booms

282

Gonets-3M No 232015 20 C2015 Mar 31.575Cylinder +2015 Mar 31.7382.48115.987879149415060.0007310

[40554]booms

282

Cosmos 2504 %2015 20 D2015 Mar 31.5752015 Mar 31.6782.48112.407716117015040.022270

[40555]2015 Mar 31.8882.49112.457717117115060.022269

2015 Mar 31.9582.48112.427716117015050.022270

2015 Jul 311191451

Breeze-KM stage *2015 20 E2015 Mar 31.575Cylinder2.6 long 2015 Mar 31.8982.49112.457717117215060.022269

[40556]6300 full2.5 dia

1320 dry

Fragments2015 20 F-L6 pieces, all in orbitFor orbital info see extra pages at the end of the year

DDragon CRS-6 #2015 21 A2015 Apr 14.840Blunt cone4.4 high2015 Apr 14.8651.6590.1766612053600.01248

R[Falcon 9v1.1][40588]36.856 days+ cylinder3.66 dia2015 Apr 14.9251.6590.0566552023510.01145

CC-LC402015 May 21.696+ 2 panels2.8 high 2015 Apr 16.8151.6492.3367673843930.0006229

8700 full16.5 span2015 Apr 17.5651.6592.5567783954030.0006223

2215 1898 cargo2015 May 21.5451.6492.4767743923990.005 172

DFalcon 9 2nd stage 2015 21 B 2015 Apr 17.840Cylinder~14 long2015 Apr 14.8651.6490.1366602063570.01148

[40589]5 days49003.66 dia2015 Apr 22.6551.6387.6065341441680.00276

2015 Apr 22

DFragments (Solar2015 21 C D 2 pieces, both have decayedFor orbital info see extra pages at the end of the year

Panel covers)

*After deploying the 3 Gonets-3M the Breeze KM stage lowered its perigee before deploying Cosmos 2504.

%Cosmos 2504 rendez-voused with the Breeze-KM stage around 2015 Apr 14 and appears to have deliberately or accidentally hit the stage, according to

reports by Anatoliy Zak at russianspaceweb.com. Lowered its orbit 2015 Jul 3.3

#Dragon CRS-6 rendezvoused with ISS 2015 Apr 17.426 and was 2017 Apr 17.455grappled by the robotic arm. Berthed 2015 Apr 17.562to Harmony nadir port.

Dragon was unberthed 2015 May 21.388 and released from the stations arm 2015 May 21.461

Thor 7 *2015 22 A2015 Apr 26.833Box + 2panels4.7 x 3.42015 Apr 29.230.931008.833332018131357520.264181

[Ariane 5 ECA][40613]> million years4600x 2.72015 Apr 30.690.101376.784099633479357550.028224

(L576 VA222)KOU-ELA324.8 span2015 May 1.600.021433.654211735732357440.000131

2015 May 1.840.031433.434211335727357420.00025

2015 May 7.800.031436.124216535778357960.0002135

Sircral 2 #2015 22 B2015 Apr 26.833Box +2 panels5.5 x 2.2No TLE issued. Geosynchronous orbit.

[40614]> million years4400x 3.1

Ariane 5 2nd stage2015 22 C2015 Apr 26.833Drum-cone3.5 long2015 Apr 29.275.92632.5824410242358210.729178

[40615]28803.94 dia

Sylda 5A upper part2015 22 D2015 Apr 26.833Barrel shaped 6.4 long2015 Apr 28.826.00630.5324358241357170.728180

[40616]517 4.6 dia

TurkmenÄlem 52E %2015 23 A2015 Apr 27.960Box +2 panels2.2 x 2.02015 Apr 27.7725.48623.8724186211354030.728179

[Falcon 9][40617]> million years4730x 4.52015 Apr 29.229.75781.33281017985354600.489179

CC-LC402015 Apr 30.751.711208.653758626775356410.118180

2015 May 1.131.721208.473758226763356450.118179

2015 May 4.140.031429.084202735623356750.000659

2015 May 5.030.031432.734209935655357850.002268

2015 May 7.100.031435.804215935775357860.0001276

2015 May 16.620.041436.134216635776357980.0003187

2015 May 21.740.071436.084216535785357870.00003232

Falcon 9 2nd stage 2015 23 B 2015 Apr 27.960Cylinder~14 long2015 Apr 27.7725.48624.3224197199354390.728179

[40618]49003.66 dia2015 Apr 29.299.75781.70281107998354640.489179

DProgress M-27M 2015 24 A2015 Apr 28.298Cyl+beehive+7.5 long2015 Apr 28.3251.5788.2765671262510.009354

[Soyuz-2 1A][40619]9.799 days+spheroid+2.72 maxdia2015 Apr 28.8751.6588.9766021872590.00585

BAI-LC1/52015 May 8.0972 panels2.3 dia2015 May 1.5651.6488.7765921822440.00596

72892015 May 4.3951.6488.4565771742220.004108

2015 May 6.5351.6488.0765571651920.002109

2015 May 7.8151.6487.3865231391510.0009128

*Norwegian maritime communication satellite for North Sea, Noewegian Sea, Red sea, Baltic Sea and the Mediterranean

#French-Italian military communication satellite

%First Turkmenistan satellite; aka MonacoSat as the sat is using an orbital slot of Monaco. 12 of the 38 transponders are fromMonaco and leased to SES.

Progress M-27M and the 3rd stage probably collided at spacecraft separation, sending Progress spinning in orbit. Progress Mm-27M decayed over the Pacific

Ocean some 800 km west of the south Chilean coast.

DSoyuz-2 1A 3rd stage2015 24 B2015 Apr 28.298Cylinder8.1 long2015 Apr 28.3251.6788.7565911233020.0148

(Block I)[40620]1 day2400?2.66 dia2015 Apr 29.0251.6587.7865441601690.000746

2015 Apr 29

Fragments2015 24 C-X20 pieces, 13 have decayedFor orbital info see extra pages at the end of the year

DOTV-4 (X-37B) $2015 25 A2015 May 20.628Cylindrical8.84 longNo TLE issued; orbits from amateur observations

R(USA 261)[40651]717.9 days+ wings2.9 high2015 May 27.6838.0290.8366943093220.001319

[Atlas V 501,AV-054)CC-LC412017 May 7.549904.5 span2015 Aug 12.0838.0390.8366943113190.0006280

2015 Oct 25.4538.0291.5367283413580.001348

2015 Oct 26.4738.0291.5367283463540.0006214

2015 Nov 19.9838.0290.8266933083210.00124

2016 Jan 5.0138.0290.8066933113170.000552

2016 May 7.1038.0391.5567293453550.0008191

2016 Aug 6.1038.0191.5767303493540.0004164

2016 Sep 17.6937.9990.9066973173210.00038

2016 Oct 11.0437.6791.5567293493530.0003159

2016 Nov 28.7037.3791.6767353543580.0003227

2016 Dec 17.8238.1191.4267233423460.0003297

2016 Dec 28.2037.9991.2867163213540.00244

2016 Mar 25.7538.0091.1067073223350.00190

2016 Apr 25.0738.0091.1067073203370.001327

USS Langley #12015 25 B2015 May 20.6283U-Cube0.31x0.10

[40652]+4 panelsx0.10

0.70 span

Opticube 01 #22015 25 C2015 May 20.6283U-Cube0.31x0.10

[40653]x0.10

Parkinsonsat #32015 25 D2015 May 20.6281.5U-Cube0.15x0.10

(PSAT-A)[40654]x0.10

Parkinsonsat #32015 25 D2015 May 20.6281.5U-Cube0.15x0.10

(PSAT-A)[40654]x0.10

BRICSat-P #42015 25 E2015 May 20.6281.5U-Cube0.15x0.10

[40655]1.9x0.10

$4th mission of the X-37B reusable spacecraft. Landed at Cape Canaveral on the former Shuttle Landing Facility runway.

#1The Unix-Space-Server Langley is a three-Unit CubeSat built and operated by the U.S. Naval Academy. It is part of a concept study looking at the feasibility of deploying a constellation of small low-cost satellites to orbit capable of TCP/IP based communications to act as Internet servers in space to provide a faster link between clients and hosts without the need for a terrestrial network.

#2, #5, #7 Three Optical CubeSats, also known as O/C-1,2,3 or OptiCube, are part of the AFSPC-05 launch. The project is sponsored through a contract by the National Reconnaissance Office and the satellites were developed and manufactured by CalPoly (PolySat). Each of the satellites uses the 3U form factor to provide small orbital targets that can be used to test orbital debris tracking technologies to improve small-object tracking in Low Earth Orbit. Current sensors can track small object with a side of ten centimeters, however, tracking of small objects becomes more difficult at lower altitudes which can have implications on Low Earth Orbit spacecraft including the International Space Station.

#3The PSAT Project (ParkinsonSAT) has been developed by students at the US Naval Academy Satellite Lab as a two-way communications transponder system that could be used to relay data from remote terminals to a global network of internet linked volunteer ground stations to speed up the return of data from remote environmental sensors, and other experiments that are installed in remote locations to the operators of the experiments.

#4BRICSat-P, known also by its full name Ballistic Reinforced Communication Satellite, is an experimental satellite mission operated by the US Naval Academy Satellite Lab to demonstrate the on-orbit operation of a Micro-Cathode Arc Thruster (µCAT). The satellite also carries on Amateur Communications Payload to be accessed by radio operators around the world.

BRICSat-P #42015 25 E2015 May 20.6281.5U-Cube0.15x0.10

[40655]1.9x0.10

Opticube 02 #52015 25 F2015 May 20.6283U-Cube0.31x0.10

[40656]x0.10

GEARRS-2 #62015 25 G2015 May 20.6283U-Cube0.31x0.10

[40657]x0.10

Opticube-03 #72015 25 H2015 May 20.6283U-Cube0.31x0.10

[40658]x0.10

Aerocube 8A #82015 25 J2015 May 20.6281.5U-Cube0.15x0.10

[40659]x0.10

Aerocube 8B #92015 25 K2015 May 20.6281.5U-Cube0.15x0.10

[40660]x0.10

Lightsail-A #102015 25 L2015 May 20.6283U-Cube0.31x0.102015 May 20.6755.0095.2069073557010.025182

[40661]+4 panelsx0.102015 Jun 10.4355.0294.1568563446110.019231

+ sail0.72 span

5.5x5.5

DAtlas-5 2nd stage%2015 25 M2015 May 20.628Cylinder12.68 long2015 May 2038916700309322

(Centaur #225)[40662]< 1 day22433.05 dia2015 May 2155956900355701

2015 May 21

#4BRICSat-P, known also by its full name Ballistic Reinforced Communication Satellite, is an experimental satellite mission operated by the US Naval Academy Satellite Lab to demonstrate the on-orbit operation of a Micro-Cathode Arc Thruster (µCAT). The satellite also carries on Amateur Communications Payload to be accessed by radio operators around the world.

#6GEARRS-2 is the second Globalstar Experiment And Risk Reduction Satellite, launched in a project operated by NearSpace Launch to investigate the use of the Globalstar satellite communications network for the command and control of a small satellite systems and CubeSats flown to Low Earth Orbit.

#8+9Aerocube 8 is part of the small satellite program of The Aerospace Corporation, El Segundo, California. The AeroCube program deploys small satellites for technical demonstrations. Each of the two AeroCube 8 satellites is 1.5 Units in size and hosts a new electric propulsion system, new nanotechnologies and new innovative solar cell technologies that are to be tested in an operational space environment.

#10LightSail-A is a 3-Unit CubeSat developed and operated by The Planetary Society to demonstrate sunlight, or rather solar pressure, as a means of spacecraft propulsion for potential future use in large sails for deep space propulsion. The LightSail-A mission will only function as a demonstration of the mechanical systems used in the deployment of the sail and validate the satellite bus for a longer test mission in a higher orbit in 2016 to actually demonstrate spacecraft acceleration through solar pressure. The sail was deployed 2015 Jun 7.824

%After the separation of OTV-4 the 2nd stage raised the apogee to around 700 km and changed the inclination for the release of the 10 Cubesats.

After the Cubesat deployment the Centaur made a deorbit-burn for destructive re-entry over the Indian Ocean.

DirecTV 152015 26 A2015 May 27.886Box +2 panels2.9x2.32015 May 27.694.36629.9824343256356730.727177

[Ariane-5 ECA][40663]> million years+4 dishesx5.92015 May 29.942.65726.55267724982358040.576179

(VA223)KOU-ELA3620042 span2015 May 31.911.61862.503001511513357590.404181

2015 Jun 1.530.901093.273515421789357630.199183

2015 Jun 2.920.131434.084212635685358090.001225

2015 Jun 10.500.111434.174212735701357960.001237

2015 Jun 14.490.111436.024216335781357880.00008235

SKY Mexico-12015 26 B2015 May 27.886Box +2 panels4.7x3x2.52015 May 27.944.34632.4824408270357890.728177

[40664]> million years+ 2 dishes span2015 May 29.922.65717.32265444592357400.587179

30002.5x2.72015 Jun 1.720.92961.553227116056357280.305180

2015 Jun 3.460.211257.383859028686357360.091186

2015 Jun 4.740.061432.304209035684357390.000738

2015 Jun 7.530.051434.304213035743357590.0002232

2015 Jun 9.240.051435.374215135762357820.0002243

2015 Jun 10.500.041436.154216635786357880.0000341

2015 Jun 12.520.051436.104216535786357870.00002180

Ariane 5 2nd stage *2015 26 C2015 May 27.886Drum-cone3.5 long2015 May 27.954.46629.7824338239356810.728179

(ESC-A)[40665]28803.94 dia

Sylda 5A upper part2015 26 D2015 May 27.886Barrel shaped 6.4 long2015 May 27.954.28632.3824405262357910.728176

[40666]517 4.6 dia

DCosmos 2505 #2015 27 A2015 Jun 5.642Cone-cyl6.3 long2015 Jun 5.7781.4289.1266091772850.00887

(Kobalt-M)[40667]105 days+2 panels2.7 maxdia2015 Jun 8.1981.4288.9866031752740.00881

[Soyuz 2-1A]PLE-43/42015 Sep 18660014.7 span2015 Jun 8.5681.4189.1766121932740.00684

2015 Jun 12.7081.4088.9766021872590.00569

2015 Jun 13.4081.4089.1766122032640.00587

2015 Jun 22.2381.4188.7765921932340.00355

2015 Jun 22.3681.4089.2366152002730.00690

2015 Jul 2.0681.4088.8065941892410.00459

2015 Jul 2.4481.4189.2066141992710.00588

2015 Jul 9.9981.4088.8765971902470.00458

2015 Jul 10.2581.4089.2066141972730.00684

2015 Jul 18.8981.4088.7765921882400.00456

2015 Jul 19.2181.3989.1766121962710.00686

2015 Jul 26.8781.3988.8765971902460.00458

2015 Jul 27.1381.3989.2766172002770.00689

2015 Aug 8.8781.3988.7065891862350.00439

2015 27 A continued on next page2015 Aug 9.0681.3989.1766121992680.00583

*After the separation of the satellites the 2nd stage began its secondary mission objective called DEMOFLIGHT to get engineering data for the future

VINCI engine that will give the 2nd stage re-start capability.

#Last film-return reconnaissance satellite.

2015 Aug 16.5381.3988.8365951902430.00453

2015 Aug 26.8081.3988.7065881912290.00391

2015 Aug 26.9981.3989.1766122062600.004153

2015 Aug 29.1581.3989.0766072042530.004146

2015 Aug 29.9681.3989.6366352043090.008156

2015 Sep 13.6881.3989.0766071912660.00698

2015 Sep 13.8781.3989.9366492053360.010136

2015 Sep 17.7981.3989.8266442053270.009120

DSoyuz 2-1A 3rd stage2015 27 B2015 Jun 5.642Cylinder6.74 long2015 Jun 5.7681.4089.0766071762800.00887

[40668]4 days23552.66 dia2015 Jun 9.7081.3887.5265301381650.00298

2015 Jun 9

Sentinel-2A2015 28 A2015 Jun 23.078Box + panel3.4x1.82015 Jun 23.1698.58100.6271667877880.00008284

[Vega] (VV 05)[40697]1140x2.352015 Jun 25.8098.57100.6071657857880.0002230

KOU-ZLV~7.5 span2015 Jul 1.0598.58100.6271677877890.0001118

AVUM stage2015 28 B2015 Jun 23.078Cylinder2 long2015 Jun 23.1798.6496.4569673957820.028199

[40698]2.18 dia2015 Jun 23.2898.6496.5269703987850.028198

Cosmos 25062015 29 A2015 Jun 23.697Cone-cyl6.5 long2015 Jun 23.8298.3193.4868231867030.03879

Kvarts (Persona 1)[40699]+4 panels2.7 dia2015 Jun 25.8598.3193.4368211916940.03772

[Soyuz 2-1B]PLE-LC 43/4~65002015 Jun 28.5298.3199.1070947077250.001314

Soyuz 2-1B 3rd stage2015 29 B2015 Jun 23.697Cylinder6.8 long2015 Jun 23.7798.3193.2268111856790.03679

[40700]

Gaofen-82015 30 A2015 Jun 26.2652015 Jun 26.3397.3094.1068534694800.0009231

[CZ-4B][40701]2015 Jun 26.4597.3094.1268554714810.0007243

TAI-LC92015 Jun 29.9397.3094.2368604794850.004330

2015 Jun 30.3897.2994.3268644844870.0002106

2015 Jun 30.4497.2994.3768674844920.000628

DCZ-4B 3rd stage2015 30 B2015 Jun 26.265Cylinder4.92 long2015 Jun 26.3297.2191.5367282274720.01815

[40702]73.758 days17002.9 dia

2015 Sep 8.023

Gaofen 8 fragments2015 30 C[43422]2018 Apr 15.8297.4193.7568364544620.0006167

2015 30 D[43423]2018 Apr 17.1197.4193.7268354514620.0008160
DProgress M-28M &2015 31 A2015 Jul 3.205Cyl+beehive+7.5 long2015 Jul 3.2351.6188.6565871892270.00375

[Soyuz-U][40713]168.727 days+spheroid+2.72 maxdia2015 Jul 3.4651.6490.0066532622870.002300

BAI-LC1/52015 Dec 19.4782 panels2.3 dia2015 Jul 5

72892015 Dec 18.5451.6492.6067813964080.0008295

DSoyuz-U 3rd stage2015 31 B2015 Jul 3.205Cylinder8.1 long2015 Jul 3.2351.6188.6265851882250.00369

[40714]days2400?2.66 dia

DMC3-1 *2015 32 A2015 Jul 10.6867-faced cyl> 2.5 long2015 Jul 10.7498.0697.6770266326630.002233

[PSLV C28][40715]+ barrel2015 Jul 10.8998.0597.7370296376630.002237

SRI-LC14472015 Jul 23.4398.0597.7570306376650.002199

DMC3-22015 32 B2015 Jul 10.6867-faced cyl> 2.5 long2015 Jul 10.8198.0597.7270286376620.002236

[40716]+ barrel2015 Jul 21.8098.0597.7070276356620.002203

4472015 Jul 25.0598.0597.6770266356590.001199

DMC3-32015 32 C2015 Jul 10.6867-faced cyl> 2.5 long2015 Jul 10.8198.0697.7070276376610.002231

[40717]+ barrel

447

CarBoNiTe1 %2015 32 D2015 Jul 10.686Cube +cyl~0.80 side2015 Jul 10.8198.0697.6770266366580.002235

[40718]91~0.50 long

~0.40 dia

DeOrbitSail #2015 32 E2015 Jul 10.6863U Cube +0.34 x 0.102015 Jul 10.9698.0597.6570256356570.002254

[40719]deployablex 0.10

sail +4 x 4

4 panels0.8 span

7

PSLV 4th stage2015 32 F2015 Jul 10.686Cylinder3.0 long2015 Jul 10.8198.1197.3370096266360.000672

[40720]2920 full1.34 dia

Progress M-28M docked 2015 Jul 5 with ISS (Pirs port). Undocked 2015 Dec 19.316 and re-entered over the south Pacific Ocean.

*Disaster Monitoring Constellation 3

#Demonstration of a satellite deorbiting sail for quicker orbital decay at the end of a satellite’s useful life.

%Technology demonstration satellite from Surrey Satellite Technology.

GPS 2F-10 (USA 262)2015 33 A2015 Jul 15.650Box +2 panels2.49x2.032015 Jul 15.8154.89729.682684820434205060.001339

[Atlas 5 401][40730]1 million years1630x2.242015 Jul 15.8355.11734.472696620450207240.005286

(AV-055)CC-LC412015 Jul 15.8954.98728.322681520425204470.0004130

2015 Jul 16.9354.98729.002683220446204600.0003328

Atlas-5 2nd stage2015 33 B2015 Jul 15.650Cylinder12.68 long2015 Jul 15.8955.27752.852741420440216310.022288

[40731]22433.05 dia2015 Jul 15.9055.36754.402745120449216960.023291

2015 Jul 19.0655.34754.472745320437217110.023291

Meteosat 112015 34 A2015 Jul 15.893Cylinder3.74 long2015 Jul 15.993.95632.7524415267358050.728178

(MSG-4)[40732]> million years20433.22 dia2015 Jul 17.730.76738.22270585744356130.552179

[Ariane 5 ECA]KOU-ELA32015 Jul 19.681.60984.753278817041357780.286359

(VA 224, L578)2015 Jul 21.232.951359.984066232802357640.036358

2015 Jul 22.213.101430.274205135562357820.003354

2015 Jul 24.003.161421.824188535376356360.00347

2015 Jul 29.093.171428.604201835589356900.00114

2015 Aug 3.163.161433.904212235689357970.001261

2015 Aug 5.803.181437.654219535442361910.009183

2015 Aug 13.923.141436.124216535785357890.0000521

2015 Aug 19.073.061436.054216435780357900.00010

Star One C42015 34 B2015 Jul 15.893Box +2 panels5.1 x 2.352015 Jul 16.003.97631.7724389264357580.728178

[40733]> million years5565 (full)x 2.22015 Jul 173442.52708.32263224150357360.600179

2015 Jul 19.601.41836.182940110316357290.432178

2015 Jul 20.370.521058.903441420340357300.224179

2015 Jul 22.280.111434.724213835727357910.0008174

2015 Jul 26.510.101435.834216035767357950.0003257

2015 Jul 28.980.091436.124216535782357910.0001134

2015 Sep 16.370.031436.084216535784357880.00005196

Ariane 5 2nd stage2015 34 C2015 Jul 15.893Drum-cone3.5 long2015 Jul 15.983.97630.5024357226357300.729179

(ESC-A)[40734]28803.94 dia2015 Jul 17.014.11633.1824426261358330.728182

Sylda 5A upper part2015 34 D2015 Jul 15.893Barrel shaped 6.4 long2015 Jul 16.003.96631.2724376261357340.728178

[40735]517 4.6 dia

MSG-4 Cooler Cover2015 34 E[40989]2015 Oct 29.472.981418.404181835301355770.00316

MSG-4 Baffle Cover2015 34 F[40990]2015 Oct 28.382.981402.774151034807354560.008302
DSoyuz TMA-17M $2015 35 A2015 Jul 22.890Cyl+beehive+7.48 long2015 Jul 23.0051.6592.5867804004020.0001290

3M[Soyuz-FG][40744]141.660 days+spheroid+2.72 maxdia2015 Dec 10.3251.6492.6267813974080.0008257

RBAI-LC1/52015 Dec 11.5502 panels2.2 dia

712010.6 span

DSoyuz-FG 3rd stage %2015 35 B2015 Jul 22.890Cylinder6.74 long2015 Jul 22.9051.6488.7265891952270.00283

(Blok I)[40745]2.2 days24102.66 dia2015 Jul 25.0751.6687.5765321491580.000746

2015 Jul 25.1

WGS-7 *2015 36 A2015 Jul 24.01Box +2 panels2015 Jul 24.0824.151325.1739965486666860.828178

[Delta IV Medium+[40746]> million years5987 full2015 Jul 24.8324.071328.1040023489668010.828178

(5,4)](#30)CC-LC37B41 span2015 Jul 25.8924.091328.1540024494667980.828178

No more TLE’s issued

Delta IV 2nd stage2015 36 B2015 Jul 24.01Cylinder12.2 long2015 Jul 24.0824.091314.1239742586661420.825179

[40747]34905.0 dia2015 Jul 24.8424.071308.1339621558659270.825179

Beidou-3 M1-S2015 37 A2015 Jul 25.520Box +2 panels2.25 x 1.02015 Jul 25.8454.98787.002823721523221930.012177

[CZ-3B/YZ-1][40748]1 million years850x 2.22015 Aug 13.3955.00773.232790621516215400.0004252

XI-LC2~17 span

Beidou-3 M2-S2015 37 B2015 Jul 25.520Box +2 panels2.25 x 1.02015 Jul 25.8554.98727.052823821526221920.012177

[40749]1 million years850x 2.22015 Jul 27.1055.01780.432807921528218730.006179

~17 span2015 Jul 28.8754.98771.882787421462215280.001348

CZ-3B 3rd stage2015 37 C2015 Jul 25.520Cylinder12.38 long2015 Jul 25.6655.00325.3015668189183900.581170

[40750]27403 dia

YZ-1 upper stage2015 37 D2015 Jul 25.520Cone + spheres2015 Jul 25.8354.89919.453132222151277360.08915

[40751]1 million years

$Soyuz TMA-17M with 3 cosmo-/astronauts (Kononenko, Yui and Lindgren)docked 2015 Jul 23.115 with ISS (Rassvet port).

The starboard solar wing did not deploy after orbit insertion, but deployed just before docking at some 5 m from ISS.

Soyuz TMA-17M undocked 2015 Dec 11.409.

*WGS-7 used its onboard motor as well ion-thrusters to raise its orbit to geosynchronous.

DKounotori 5 #2015 38 A2015 Aug 19.493Cylinder10.06 long2015 Aug 19.6151.6989.3566211853000.009312

(HTV 5)[40873]41.39 days158764.27 dia2015 Aug 19.9251.6889.9866522463000.004308

[H-2B]TAN-LC22015 Sep 29.8812020 empty 2015 Aug 23.0051.6491.9367483593790.001191

2015 Sep 29.5251.6592.5567783954040.0006343

Intelsat 342015 39 A2015 Aug 20.863Box +2 panels5.6 x 3.52015 Aug 20.654.70631.3824380243357590.728179

[Ariane 5 ECA][40874]> million years3300x 3.02015 Aug 22.541.77803.93286408748357750.472178

(VA225, L579)KOU-ELA31800 empty2015 Aug 23.630.271139.503613923748357720.166174

2015 Aug 25.370.071324.103994331338357910.056155

2015 Aug 28.230.061432.024208535613357990.00256

2015 Aug 31.760.041436.174216635772358030.0004238

2015 Sep 2.070.051436.124216535770358030.0004236

2015 Sep 16.750.021437.704219635813358220.0001224

2015 Sep 30.440.011436.054216435777357940.000276

2015 Oct 1.490.011436.174216635779357960.0002224

Eutelsat 8 West B2015 39 B2015 Aug 20.863Box +2 panels5.5 x 22015 Aug 20.664.70633.5724436249358660.729178

[40875]> million years5782x 2.22015 Aug 22.502.22767.27277627021357470.517179

2015 Aug 23.071.251046.403414219779357490.234176

2015 Aug 31.680.081436.104216535766358070.0005246

2015 Sep 17.090.051436.074216435785357870.0000361

Ariane 5 2nd stage2015 39 C2015 Aug 20.863Drum-cone3.5 long2015 Aug 20.664.73632.1524399235358060.729179

(ESC-A)[40876]28803.94 dia

Sylda 5A upper part2015 39 D2015 Aug 20.863Barrel shaped 6.4 long2015 Aug 20.664.73631.2524376238357580.729179

[40877]517 4.6 dia

Yaogan 272015 40 A2015 Aug 27.1052015 Aug 27.16100.46107.937510106212010.0099

[CZ-4C][40878]10402015 Aug 27.23100.46108.007513106412050.00911

WUZ2015 Aug 27.92100.50109.427578119412060.0008273

CZ-4C 3rd stage2015 40 B2015 Aug 27.105Cylinder4.9 long2015 Aug 27.91100.45108.007513106412040.00910

[40879]17602.9 dia

Fragments2015 40 C[43424]2018 Apr 15.96100.35109.927602110813380.015251

2015 40 D[43425]2018 Apr 16.64100.42108.937556107012850.014231

#HTV 5 rendez voused with ISS 2015 Aug 24.430 and was grappled by the station’s robotic arm 2015 Aug 24.436 and berthed 2015 Aug 24.539 to the nadir port

of the Harmony module. Unberthed 2015 Sep 28. And 2015 Sep 28.703 released by stations robotic arm.

The H-2B 2nd stage made a cold gas de-orbit manoeuvre at the end of the 1st orbit and decayed over the Pacific Ocean

GSAT-62015 41 A2015 Aug 27.474Box +2 panels2.1 x 2.52015 Aug 28.987.49795.35284368384357310.481179

[GSLV Mk. II D6)[40880]> million years+ mesh antennax 4.12015 Sep 1.821.191431.284207135671357130.0005230

Stage)SRI-LC2985 dry~109.6 span2015 Sep 5.881.171434.584213535676358370.002358

2117 full6 dia2015 Sep 7.851.181436.024216335758358110.0006314

2015 Sep 16.951.161436.074216435750358210.0008335

DGSLV 3rd stage2015 41 B2015 Aug 27.474Cylinder8.7 long2015 Aug 28.1519.98628.3324301155356900.731179

(CUS=Cryogenic Upper[40881]917.3 days2.8 dia2018 Mar 1.0420.0590.9266981175220.030115

Stage)2018 Mar 1.8

Inmarsat 5-F32015 42 A2015 Aug 28.489Box +2 panels6.98x3.592015 Aug 29.7626.631377.67410134369649010.738180