Year of Launch 2016RAE Table of Earth Satellites(Issued 2016)Page 1

NameCospar IDLaunch dateShape andSizeDate of OrbitalNodalSemiPerigeeApogeeOrbitalArgument

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

FragmentCospar ID[Norad#]determination(deg)(min)(km)(km)(km)(deg)

Belintersat 12016 01 A2016 Jan 15.706Box +2 panels2.36x2.102016 Jan 15.8026.38750.9327367197417810.760179

[CZ-3B/E][41238]> million yearsx3.602016 Jan 28.800.061436.104216535779357940.000233

XI-LC3~152016 Feb 3.810.041436.074216435778357930.000244

2016 Feb 18.800.011436.104216535779357930.000223

DCZ-3B/E 3rd stage2016 01 B2016 Jan 15.706Cylinder12.38 long2016 Jan 15.8426.27709.8326359158398040.752178

[41239]171 days27403 dia2016 Jul 4.3926.0590.436674924990.03180

2016 Jul 4

Jason-32016 02 A2016 Jan 17.779Box +2 panels~3 x1.02016 Jan 17.8566.05111.757686129513200.002234

[Falcon-9 v1.1][41240]553x1.02016 Jan 18.0666.04111.857690130013230.001228

(F9-021)VDB-SLC4E10 span2016 Feb 4.8066.04112.507720133713460.0005282

2016 Feb 5.7466.04112.657727134213550.0008268

DFalcon 9 v1.12016 02 B2016 Jan 17.779Cylinder13 longDe-orbited in first orbit. Entered between Hawaii and Aleutian Islands.

2nd stage[NNA]~ 0.05 d~4000-45003.66 diaDecay observed from Hawaii.

2016 Jan 17.82

The Falcon-9 1st stage made a soft landing on the droneship OCISLY in the Atlantic Ocean.

IRNSS-1E2016 03 A2016 Jan 20.168Box +2 panels1.58x1.502016 Jan 20.2519.19361.3516805288205660.603178

[PSLV XL](C31)[41241]> million years1425 fullx1.502016 Jan 21.6219.16634.5824462345358210.725180

SRI-LC2603 dry~5 span2016 Jan 22.6024.04775.15279527357357900.509180

2016 Jan 25.5528.051425.934199635347358270.006181

2016 Jan 27.7028.031428.204201035431358320.005186

2016 Jan 28.4728.041431.584207735575358200.003184

2016 Feb 9.8328.061436.054216435697358740.002185

2016 Feb 19.9828.071436.124216535696358770.002184

PSLV 4th stage2016 03 B2016 Jan 20.168Cylinder2.6 long2016 Jan 20.2619.07366.9216978289209100.607179

[41242]1.34 dia

Intelsat 29e2016 04 A2016 Jan 27.972Box +2 panels6 x 32016 Jan 27.950.62627.5724281280355250.726194

[Ariane 5-ECA][41308]> million years6552 fullx 22016 Feb 2.300.48647.77248001288355540.691179

(VA228, #84)KOU-ELA32950 dry~50 span2016 Feb 3.690.33718.92265844747356630.581186

2016 Feb 5.310.31835.952939610302357330.433184

2016 Feb 6.950.161094.123517321829357590.198198

2016 Feb 8.240.161337.804021831897357820.048198

2016 Feb 9.890.131416.174177435005357860.009191

2016 Feb 11.640.121435.974216235783357840.00002176

2016 Feb 16.340.121436.134216635781357930.0001328

Ariane 5 2nd stage2016 04 B2016 Jan 27.972Cylinder5.84 long2016 Jan 27.950.53628.0524284275355550.726178

(ESC-A + VEB)[41309]56685.4 dia

Eutelsat 9B2016 05 A2016 Jan 29.930Box +2 panels 7.5 high2016 Jan 30.0849.03633.8524443442356860.7210

[Proton-M/Breeze-M][41310]> million years5612> 30 span2016 Jan 30.5512.05711.83264094374356860.5930

(#410)BAI-LC200/392016 Feb 8.180.061430.504205535638357160.00092

2016 Feb 8.760.071431.404207335649357400.001189

2016 Feb 9.130.071433.354211135669357960.002179

2016 Feb 9.880.071436.084216535768358040.0004320

2016 Feb 10.260.071436.304216935786357940.00009294

2016 Feb 13.840.061436.124216535786357870.000227

Breeze-M stage2016 05 B2016 Jan 29.930Stubby Cyl2.62 long2016 Jan 30.5712.53663.65252033755338940.5982

[41311]1220~2.4 dia

Breeze-M tank2016 05 C2016 Jan 29.930Torus2.1 long2016 Jan 30.0849.40346.4016339348195720.588354

[41312]12904.1 dia

0.8 cross

Beidou M3-S (#21)2016 06 A2016 Feb 1.312Box +2 panels2016 Feb 1.6155.00782.352812521512219810.008177

[CZ-3B3C/YZ-1](Y14)[41315]> million years42002016 Feb 3.5655.01782.952814021531219910.008174

XI-LC21014 dry

YZ-1 upperstage2016 06 B2016 Feb 1.312Cone +spheres2016 Feb 1.6255.17899.653087121870271150.08519

[41316]

CZ-3B 3C 3rd stage2016 06 C2016 Feb 1.312Cylinder12.38 long2016 Feb 3.4955.01326.1815697220184160.580169

[41325]27403 dia

GPS IIF-12 (USA 266)2016 07 A2016 Feb 5.568Box +2 panels2.49x2.032016 Feb 5.3255.04728.472681920438204420.0009111

[Atlas 5 401][41328]1 million years1630x2.242016 Feb 12.4155.03728.672682320437204520.0003302

(#61, AV-057)CC-LC41~ 15 span

Atlas-5 2nd stage2016 07 B2016 Feb 5.568Cylinder12.68 long2016 Feb 5.3155.22744.232720420450212010.014287

(Centaur)[41329]22433.05 dia

Cosmos 25142016 08 A2016 Feb 7.015Cylinder3.7 long2016 Feb 7.2164.80676.332552319132191580.0005230

(Glonass-M 51)[41330]1 million years+ box2.4 dia2016 Feb 11.5264.80678.272557219156192300.00141

[Soyuz 2-1B/Fregat-M]PLE-43/4+ 2 panels7.2 span

Fregat-M stage2016 08 B2016 Feb 7.015Spheres ring1.55 long2016 Feb 7.0864.78683.002569119155194680.00664

[41331]930 dry3.35 dia

6710 full

Kwangmyongsong-4 *2016 09 A2016 Feb 7.020Box +2 panels~ 1 side2016 Feb 7.1597.5394.2768624665000.003339

[UNHA-3][41332]150-200~3 span

UNHA-3 3rd stage2016 09 B2016 Feb 7.020Cylinder3.7 long?2016 Feb 7.4697.5493.9368454325010.005336

[41333]1.2 dia?

*Shape from picture on North Korean television. Size estimated from recovered payload fairing by South Korea; cylinder-cone, 1.25 dia, 1.1 + 0.85 high.

FIA-Radar 42016 10 A2016 Feb 10.4862016 Feb 11.19122.99103.857460107510860.0007246 #

(NROL-45, USA 267)[41334]2016 Feb 12.46122.97106.877460107710850.0006355

[Delta IV Medium+]VDB-SLC6

(5,2)(#31)

Delta IV 2nd stage2016 10 B2016 Feb 10.486Cylinder13.7 longDe-orbited orbit in Indian Ocean

[NNA]34905.0 dia

#No TLE issued; orbits from amateur observations.

Sentinel-3A2016 11 A2016 Feb 16.748Box + panel2.20x2.212016 Feb 16.8398.62100.9371818018040.000257

[Rockot/Breeze-KM][41335]1244 fullx3.712016 Feb 16.8798.62100.9571828018060.000377

PLE-LC133/31124 dry10.5 m2

Breeze-KM stage2016 11 B2016 Feb 16.748Cyl+Cone2.6 long2016 Feb 16.8798.6996.2569584147440.024309 $

[41336]13202.5 dia

$Disposal orbit after satellite release.

Hitomi %12016 12 A2016 Feb 17.365Otagonal cyl6 long2016 Feb 17.3831.0195.9569435515780.002329

(Astro-H)[41337]+ cyl +boom6 long2016 Feb 17.5231.0196.0269465545810.002329

[H-IIA] (H202, F30)TAN+2 panels~ 9 span2016 Feb 17.8231.0196.1269515655800.001282

2700

ChubuSat 2 %22016 12 B2016 Feb 17.365Box0.58x0.552016 Feb 17.8231.0096.0569485595790.001296

(Kinshachi 2)[41338]50x0.50

Chubusat 3 %22016 12 C2016 Feb 17.365Box0.58x0.552016Feb 17.8331.0196.0369475585780.001302

(Kinshachi 3)[41339]50x0.50

2016 12 continued on next page

*Shape from picture on North Korean television. Size estimated from recovered payload fairing by South Korea; cylinder-cone, 1.25 dia, 1.1 + 0.85 high.

#No TLE issued; orbits from amateur observations.

$Disposal orbit after satellite release.

%1Japanese astronomical satellite o study X-rays and gamma-rays from galaxy clusters. On 2016 Mar 28 Space-Track announced a breakup notice: Astro H at approximately 2016 Mar 26.347 with 5 associated pieces as of 2016 Mar 27.583; further analyses pin point the event at 2016 Mar 26.07. JAXA announced in a press briefing that Astro-H went into a fast roll due to false readings of Internal Reference Unit after a re-orientation maneuver on March 25.765.

%2ChubuSat-2/3, informally called Kinshachi-2/3, are two microsatellites part of a project of Nagoya and Daido Universities and several aerospace companies located in the Chubu region of Japan. The mission demonstrates a cost-effective satellite platform and an imaging payload that will make observations of Earth in visible and infrared wavelengths, track space debris and serve outreach purposes by relaying messages via the amateur radio bands.

Horyu 4 %32016 12 D2016 Feb 17.365Box0.434x0.3132016 Feb 17.8331.0096.026946557 578 0.002 307

[41340]10x0.429

H-IIA 2nd stage2016 12 E2016 Feb 17.365Cylinder9.2 long2016 Feb 17.7630.6295.7769345435680.002302

[41341]4 dia

DFragment2016 12 F2016 Feb 17.3652016 Feb 19.0831.0196.0869505635790.001291

H-IIA 2nd stage[41342]347 days2017 Jan 24.9730.9991.0767063153390.002299

2017 Jan 29

Fragments (Hitomi)2016 12 G-RT120 pieces, 2 have decayedFor orbital information see ectra pages at end of year

3Horyu-4 is a small technology demonstration satellite built by the Kyushu Institute of Technology. It is also known as AEGIS – Arc Event Generator and Investigation Satellite

SES 92016 13 A2016 Mar 4.983Box +2 panels2016 Mar 4.7627.96730.5326869334406480.750178

[Falcon 9 FT][41380]> million years53302016 Mar 7.5827.98749.9327343328416000.755180

(F9-022)2016 Mar 9.7514.16852.97297935223416060.611181

2016 Mar 14.680.441405.604156628570418050.159204

2016 Mar 16.710.171436.184216730483410920.126289

2016 Mar 21.560.161435.824216030631409300.122275

2016 Mar 23.830.171437.404219030885407390.117276

2016 Mar 25.920.141438.234220731087405690.112276

2016 Apr 2.880.171437.184218630356412590.129268

2016 Apr 7.140.121435.954216232989385770.066281

Falcon 9 FT 2nd stage2016 13 B2016 Mar 4.983Cylinder14.3 long2016 Mar 4.7627.95730.4326867322406540.751 178

[41381]40003.66 dia

Eutelsat 65W A2016 14 A2016 Mar 9.222Box +2 panels7.9x3.22016 Mar 9.300.50632.4224406229358250.729177

[Ariane 5][41382]6564x3.62016 Mar 10.590.10760.88276096678357810.527173

(VA 229; #85)KOU-ELA32016 Mar 11.600.011075.823477921023357790.212109

2016 Mar 11.720.001076.423479221049357770.21286

2016 Mar 13.720.021388.984123733965357530.022179

2016 Mar 14.580.031434.984214335727358010.0009265

2016 Mar 14.920.031433.934212335729357590.0004233

2016 Mar 18.350.031435.524215435761357890.0003200

2016 Mar 19.620.031436.054216435780357910.0001275

Ariane 5 2nd stage2016 14 B2016 Mar 9.222Cylinder6.26 long2016 Mar 9.300.52629.9824343237356920.728183

(ESC-A +VEB)[41383]45405.4 dia2016 Mar 9.540.44628.7824312220356470.729173

3Horyu-4 is a small technology demonstration satellite built by the Kyushu Institute of Technology. It is also known as AEGIS – Arc Event Generator and Investigation Satellite

IRNNS-1F2016 15 A2016 Mar 10.438Box +2 panels1.58x1.502016 Mar 10.4917.88362.4516839271206500.605178

[PSLV-XL C32][41384]1425x1.502016 Mar 12.679.77825.95291619796357680.445181

SRI603 dry~ 5 span2016 Mar 13.865.281373.104092333348357400.029182

2016 Mar 21.135.091435.424215135692358540.002163

2016 Mar 23.215.091436.124216535700358740.002173

PSLV 4th stage2016 15 B2016 Mar 10.438Cylinder2.60 long2016 Mar 10.3217.74368.0717013271209980.609178

[41385]9202.02 dia

Resurs P32016 16 A2016 Mar 13.789Cone-Cyl7.93 long2016 Mar 13.8797.2991.8567442794520.01357

[Soyuz-2.1B][41386]+2 panels2.72 maxdia2016 Mar 15.7997.2891.8567442804500.01352

BAI-LC31/65730~ 13 span2016 Mar 18.5397.2893.1568083894690.00688

DSoyuz-2.1B2016 16 B2016 Mar 13.789Cylinder6.74 long2016 Mar 13.8797.3091.8067412834420.01261

3rd stage[41387]195 days23552.66 dia2016 Sep 24.4697.2887.0565071231330.0008280

2016 Sep 24

ExoMars 2016 *2016 17 A2016 Mar 14.397Box +2 panels3.2 x 22016 Mar 14.00551.5175175

[Proton-M/Breeze-M][41388]x22016 Mar 14.4622705800

(#411)BAI-LC200/39373217.5 span2016 Mar 14.57251.669721086

Double Cone1.8 high2016 Mar 14.834 Trans-Martian Injection

6002.4 dia2016 Oct 1929895856%

2016 Nov 254.2 days 230-31061000%

Breeze-M stage #2016 17 B2016 Mar 14.397Cylinder2.61 longAttached to 2016 17 A till 2016 Mar 14.842

[41389]23704.0 diaIn heliocentric orbit

Breeze-M tank2016 17 C2016 Mar 14.397Torus2.1 long2016 Mar 14.6851.60376.4217269696210860.590100

[41390]12904.1 dia

0.8 cross

*ExoMars 2016 consists of the Trace Gas Orbiter and the Schiaparelli Lander. It is a joint ESA/Russian mission.

The Schiaparelli Lander will land 2016 Oct 19 in Meridiani Planum at 6°W and 2°S using aero breaking, parachute and propulsive landing system.

The landing site is just NW of Endeavour Crater, where since 2011 Opportunity rover is exploring.

On 2016 Oct 16 the lander separated from the orbiter. On 2016 Oct 19 the radiosignals stopped just before landing.

%Mars orbits. Using aerodynamic drag the orbit will be lowered to around 400 km circular by the end of 2017.

#After spacecraft separation the stage made a pair of avoidance manoeuvres to get away from Exomars and also missing Mars.

Based on photos taken by the OASI observatory in Brazil is seems that the Breeze-M stage broke up after the 1st avoidance burn. Six large pieces and several smaller are visible on the photos close to ExoMars.

DSoyuz TMA-20M $2016 18 A2016 Mar 18.893Cyl+beehive+7.48 long2016 Mar 18.8951.6588.7365901932300.003103

3M[Soyuz-FG][41391]172.158 days+spheroid+2.72 maxdia2016 Mar 19.0251.6789.6766372023140.008188

BAI-LC1/52016 Sep 7.0512 panels2.2 dia2016 Mar 19.0951.7490.8066922064210.016320

716710.6 span2016 Mar 22.5051.6492.6567834034050.0002346

2016 Sep 6.6751.6592.6367824014050.0003301

DSoyuz-FG 3rd stage2016 18 B2016 Mar 18.893Cylinder6.74 long2016 Mar 18.8951.6488.6265851962170.00292

(Blok I)[41392]2.2 days24102.66 dia2016 Mar 21.0951.6487.5365311451600.001151

2016 Mar 21

$Soyuz TMA-20M docked 2016 Mar 19.173 with ISS (Poisk port) with 2 cosmonauts (Ovchinin and Skripochka) and 1 astronaut (Jeff Williams).

Undocked 2016 Sep 6.910

DCygnus OA-6 *2016 19 A2016 Mar 23.129Cylinder +26.39 long2016 Mar 23.1551.6589.1866132312370.0004289

(S.S. Rick Husband)[41393]91.428circular panels 3.07 dia2016 Mar 23.4551.6689.4066242402500.0007244

[Atlas V 401]CC-LC412016 Jun 22.5571800 dry2016 Mar 25.0751.6590.9767012503930.01198

(AV 064)7495 full2016 Mar 26.2951.6592.5867793984040.000510

3395 cargo2016 Mar 26.4351.6492.6867854034080.000411

2016 Jun 13.6251.6492.6267824034030295

2016 Jun 14.7151.6492.6767844024090.0004356

2016 Jun 14.9151.6492.7367874054110.000439

2016 Jun 15.1651.6192.7267863984170.00137

2016 Jun 15.8651.6492.3267673873890.0002157

2016 Jun 22.2151.6492.3267663873890.0001158

DLemur-22016 19 B2016 Jun 20213U-Cube0.34x0.102016 Jun 21.7151.6492.3867703883940.000442

BRIDGEMANDRMUZZ[41595]361 days+2 panelsx0.102017 Jun 25.7451.6187.6265351501610.0008318

2017 Jun 25.90854.60.54 span

DLemur-22016 19 C2016 Jun 20213U-Cube0.34x0.102016 Jun 21.7751.6492.3867703873950.000539

BRIDGEMAN DRMUZZ[41596]260 days+2 panelsx0.102017 Mar 8.1051.6587.6365361541610.000647

2017 Mar 8.19554.60.54 span

DLemur-22016 19 D2016 Jun 20213U-Cube0.34x0.102016 Jun 21.6451.6492.3867703893940.000347

CUBECHEESE NATE[41597]258 days+2 panelsx0.102017 Mar 6.4151.5987.3865231351530.001342

2017 Mar 6.46554.60.54 span

DLemur-22016 19 E2016 Jun 20213U-Cube0.34x0.102016 Jun 21.7751.6492.3867703893940.000444

CUBECHEESENATE[41598]251 days+2 panelsx0.102017 Feb 27.4851.6187.5565321491570.0006312

2017 Feb 27.57154.60.54 span

$Soyuz TMA-20M docked 2016 Mar 19.173 with ISS (Poisk port) with 2 cosmonauts (Ovchinin and Skripochka) and 1 astronaut (Jeff Williams).

Undocked 2016 Sep 6.910

*Cygnus OA-6 rendezvoused with ISS 2016 Mar 26.442 and was captured 2016 Mar 26.451 by the stations robotic arm.

Berthed 2016 Mar 26.609 to ISS (Unity nadir port). The 3395 3279 kg cargo includes 20 Flock-2e 3U-Cubesats to be deployed from the ISS.andFive 5 Lemur-2 3U-Cubesats from Cygnus. Unberthed 2016 Jun 14.488 and at 2016 Jun 14.563 released from the robotic arm. The SAFFIRE experiment (fire experiment inside a bosx in the Cygnus)was conducted and on 2016 June 20 21 4 of the 5 Lemur-2 Cubesats were released, one failed to deploy.

Cygnus OA-6 was de-orbited over the Pacific Ocean.

The Atlas-5 2nd stage(Centaur)was de-orbited in first orbit over the Ocean south of Australia.It decayed farther east than predicted due to a minute

longer burn of the Centaur caused by a 5 sec shorter burn of the 1st stage. It ran out of fuel during the de-orbit burn.

Cosmos 25152016 20 A2016 Mar 24.404Cone+box4.0x2.32016 Mar 24.4697.6593.2368113265390.01673

(Bars-M #2L)[41394]+2 panelsx2.3

[Soyuz 2-1A]PLE-LC43/44000

Soyuz 2-1A 3rd stage2016 20 B2016 Mar 24.404Cylinder6.74 long2016 Mar 24.4697.6493.2568123265410.01674

[41395]23552.66 dia

Beidou-2I 62016 21 A2016 Mar 29.841Hexahedral2.2x1.72016 Mar 30.0455.04631.2824377200357970.730175

[CZ-3A][41434]> million years+2 panelsx2.0

XI-LC2> 2000

CZ-3A 3rd stage2016 21 B2016 Mar 29.841Cylinder12.38 long2016 Mar 30.0854.96625.0724217225354520.727175

[41435]27403.0 dia

DProgress MS-02 &2016 22 A2016 Mar 31.683Cyl+beehive+7.5 long2016 Mar 31.6851.6588.5565811882170.00263

[Soyuz 2-1A][41436]196.886 days+spheroid+2.72 maxdia2016 Mar 31.8751.6489.8066432612670.0005185

BAI-LC31/62016 Oct 14.5692 panels2.3 dia2016 Apr 2.4451.6589.8766462662690.000297

72892016 Apr 2.7051.6492.6367824024050.000230

2016 Oct 13.3851.6492.6567833994090.000768

DSoyuz 2-1A 3rd stage2016 22 B2016 Mar 31.683Cylinder6.74 long2016 Mar 31.6851.6388.4765771802170.00384

[41437]3.552 days23552.66 dia2016 Apr 3.1861.6587.1065091251360.0008141

2016 Apr 3.235

Progress MS-02 docked 2016 Apr 2.749 with ISS (Zvezda aft port). Undocked 2016 Oct 14.401

DShijian-10#2016 23 A2016 Apr 5.735Cyl-cone2016 Apr 5.9942.8989.5266292342670.003320

R[CZ 2D][41448]12.619 days36002016 Apr 9.3442.8989.4866282322660.003338

(#Y36) JIUQ-LC43/6032016 Apr 18.3542016 Apr 18.4342.9089.7066392532660.00150

DCZ 2D 2nd stage2016 23 B2016 Apr 5.735Cylinder10.9 long2016 Apr 6.0442.8989.5266292332680.003315

[41449]13 days60503.35 dia2016 Apr 18.7442.8987.4865281501500325

2016 Apr 18

DSJ-10 Orbital module2016 23 E2016 Apr 5.735CylinderCylinder2016 Apr 18.6642.8989.7266392532690.00148

[41455]87 days2016 Apr 22.8342.8990.1366592543080.00463

2016 Jul 12016 Jul 1.4142.8987.1865141311390.0006260

Fragments2016 23 C-D, F 3 pieces, 2 have decayedFor orbital information see extra pages at end of the year.

Progress MS-02 docked 2016 Apr 2.749 with ISS (Zvezda aft port). Undocked 2016 Oct 14.401

#The re-entry capsule separated 2016 Apr 5.340 from the orbital module and soft-landed in Inner Mongolia. The orbital module became 2016 23 E.

DDragon CRS 8 *2016 24 A2016 Apr 8.863Blunt cone4.4 high2016 Apr 8.8851.6690.1366602093530.01144

R[Falcon 9 FT][41452]32.925 days+ cylinder3.66 dia2016 Apr 9.0051.6590.2066622123560.01147

(F9-23)CC-LC402016 May 11.788+ 2 panels2.8 high 2016 Apr 9.6951.6591.6267333513570.000517

10400 full16.5 span2016 Apr 10.0051.6492.4267723913950.000350

3136 3059 cargo2016 May 10.5651.6492.6267824024040.0002 109

DFragments2016 24 B-C 2 pieces, both have decayedFor orbital information see extra pages at end of the year.

*CRS-8 (Dragon capsule) rendezvoused 2016 Apr 10.445 with ISS; was grappled 2016 Apr 10.474 by the stations robot arm and berthed 2016 Apr 10.581 to Harmony nadir port. The trunk section carried the 1413 kg Bigelow Expandable Activity Module. It was 2016 Apr 16.260 removed from the trunk section and

was 2016 Apr 16.400 berthed to ISS (Tranquility aft port) by the robotic arm. BEAM will remain there for about 2 years for testing the concept.

The Falcon 9 2nd stage was de-orbited over the Indian Ocean south of Australia.

Dragon CRS-8 was unberthed 2016 May 11.460 from the Harmony module by the robotic arm and placed in its release position. Relase came at 2016 May 11.55

and the capsule landed in the Pacific Ocean about 370 km SW of Long Beach, California.

Sentinel-1B $12016 25 A2016 Apr 25.876Box +2 panels2.8 x 2.52016 Apr 25.9698.1998.7270766937010.000595

[Soyuz2-1A(ST-A)][41456]+ SARpanelx 42016 Apr 30.1398.1898.7270766957000.000365

(VS 14)KOU-ELS2170 dry20.7 span

2300 full12 long

MicroSCOPE $22016 25 B2016 Apr 25.876Box +2 panels0.138x0.1042016 Apr 26.1898.2399.0370917117150.000388

[41457]330x1.158

OUFITI-1 $32016 25 C2016 Apr 25.8761U Cube0.10x0.102016 Apr 26.9598.2295.9569434426860.018238

[41458]10.10

E-ST@R II $42016 25 D2016 Apr 25.8761U Cube0.10x0.102016 Apr 26.9598.2295.9569434426860.018239

[41459]10.10

AAUSAT-4 $52016 25 E2016 Apr 25.8761U Cube0.10x0.102016 Apr 27.0298.2295.9569434426860.018238

[41460]10.10

2016 25 continued on next page

was 2016 Apr 16.400 berthed to ISS (Tranquility aft port) by the robotic arm. BEAM will remain there for about 2 years for testing the concept.

The Falcon 9 2nd stage was de-orbited over the Indian Ocean south of Australia.

Dragon CRS-8 was unberthed 2016 May 11.460 from the Harmony module by the robotic arm and placed in its release position. Relase came at 2016 May 11.55

and the capsule landed in the Pacific Ocean about 370 km SW of Long Beach, California.

$1The Sentinel-1B mission is a European Radar Observatory mission designed and developed by ESA for operation by the European Commission under the Copernicus program. Sentinel-1B will provide continuity of C-Band Synthetic Aperture Radar data for operational applications across Europe and to contribute to the GEOSS (Global Earth Observation System of Systems).

$2A minisatellite mission of the French and European Space Agencies with involvement of a number of European institutions to conduct a fundamental physics experiment testing the General Theory of Relativity to gather data on the Weak Equivalence Principle (WEP) which postulates that a perfect proportionality

exists between the inertial mass and the gravitational mass of a body.

$3Orbital Utility for Telecommunication Innovation from the University of Liege (B)with a Digital Smart Technilogies for Amateur Radio system.

$4From the Politecnico di Torino, Turin, Italy to the demonstration of an autonomous active attitude control system based on magnetic actuators.

$5Aalborg University Cubesat 4 is student built with a Automatic Identification System receiver.

ASAP-S adapter $62016 25 F2016 Apr 25.876Hollow Cyl2016 Apr 26.3198.2295.9869454426900.018241

[41461]+3 petals

DFregat M upperstage2016 252016 Apr 25.876Cylinder6.74 long2016 Apr 25.89298.2686686 Sentinel-1B deploy

[NNA]~ 0.25 day23552.66 dia2016 Apr 25.95998.2453665 Cubesat deploy

2016 Apr 26.1 2016 Apr 26.06498.2711711 MicroSCOPE deploy

De-orbited into south Atlantic Ocean after deploying the satellites

exists between the inertial mass and the gravitational mass of a body.

$3Orbital Utility for Telecommunication/Technology Innovation from the University of Liege (B)with a Digital Smart Technilogies for Amateur Radio system.

$4From the Politecnico di Torino, Turin, Italy to the demonstration of an autonomous active attitude control system based on magnetic actuators.

$5Aalborg University Cubesat 4 is student built with a Automatic Identification System receiver.

$6Adapter in between Fregat stage and Sentinel-1B. Inside the ASAP was the MicroSCOPE satellite and on one of the petals the launch box of the 3 Cubesats was mounted.

Lomonosov*12016 26 A2016 Apr 28.084Box +2016 Apr 28.2997.2794.1868574714860.001257

(MVL-300)[41464]truss

[Soyuz 2-1A]VOS-1S #+2 panels

645

AIST-2D *22016 26 B2016 Apr 28.084Box +2 panels~ 2 long2016 Apr 28.2997.2794.1768574704860.001259

[41465]531x~1 x~1

~7 span

SamSat-218D *32016 26 C2016 Apr 28.0843U Cube0.34x0.102016 Apr 28.2997.2794.1768574714850.001257

[41466]4x0.10

DSoyuz 2-1A 3rd stage2016 26 D2016 Apr 28.084Cylinder6.74 long2016 Apr 30.2897.3088.3865731872020.001321

[41467]2.374 days23552.66 dia2016 Apr 30.2897.2987.3765231371510.001298

2016 Apr 30.458Re-entered over the Atlantic Ocean off the coast of southern Africa.

DVolga upperstage2016 26 E2016 Apr 28.0842016 Apr 28.2997.2794.1568564704850.004264

[41468]0.287 dayDe-orbited into Pacific Ocean after deploying the satellites

2016 Apr 28.371

$6Adapter in between Fregat stage and Sentinel-1B. Inside the ASAP was the MicroSCOPE satellite and on one of the petals the launch box of the 3 Cubesats was mounted.

#Inaugural launch from Vostochny (Eastern) Cosmodrome, the new Russian Launch Complex in the far east of Siberia near the Chinese border at 51°53’04.39”N 128°20’05.2E in Amur Oblast. It is an expansion from the old Svobodny Missile Range.

*1Mikhailo Lomonosov, also known as MVL-300, is a Russian Astro- and Geophysics satellite named after 18th century scientist Mikhail Vasilyevich Lomonosov. The spacecraft, operated by Moscow State University, is outfitted with seven instruments for a range of measurements including X- and Gamma-Ray detection, charged particle influx, radiation dose, and electromagnetic fields.

*2AIST-2D is a technology demonstration and scientific research satellite developed at Samara Aerospace University in cooperation with satellite manufacturer TsSKB-Progress. The satellite hosts eight payloads dedicated to technology demonstrations and scientific research.

*3The SamSat-218/D demonstrator satellite is developed by students at the Samara State University as an educational and technology demonstration project.

IRNSS-1G2016 27 A2016 Apr 28.305Box +2 panels1.58x1.502016 Apr 28.3817.86362.3216836276206390.605178

[PSLV XL](C33)[41469]> million years1425 fullx1.502016 Apr 29.6317.83633.6324438302358160.726180

SRI-LC1603 dry~5 span2016 May 2.415.701268.103880929044358170.087181

2016 May 3.365.101422.354189535212358510.007182

2016 May 6.695.071428.324201235435358330.005163

2016 May 7.705.081430.554205635575357810.002144

2016 May 8.955.021437.184218635761358540.001103

2016 May 11.435.001435.734215835748358100.0007139

2016 May 16.425.061436.034216435774357970.0003142

PSLV 4th stage2016 27 B2016 Apr 28.305Cylinder2.6 long2016 Apr 28.3817.76366.9816980276209260.608179

[41470]1.34 dia2016 Apr 28.4517.75667.1516985276209360.608179

JCSat-142016 28 A2016 May 6.223Box +2 panels2016 May 6.0323.70634.1524451188359560.731179

[Falcon 9 FT][41471]> million years2180 dry2016 May 10.470.281379.254104533467358650.029172

(F9-24)CC-LC404696 full2016 May 11.500.051437.404219035761358620.00138

2016 May 16.550.021436.074216435773357980.000364

2016 May 20.840.011436.074216435775357960.000269

2016 Jun 4.710.011441.554227135890358960.00008296

2016 Jun 21.460.021436.124216535769358040.0004116

2016 Jun 30.400.021436.104216535775357980.0003178

Falcon 9 2nd stage2016 28 B2016 May 6.223Cylinder14.3 long2016 May 6.0323.73633.1724426187359070.731179

[41472]40003.66 dia

Yaogan 302016 29 A2016 May 15.113Box +2 panels2016 May 15.1298.2398.7070756907030.001256

[CZ-2D][41473]2016 May 15.1898.0797.5270196256550.002234

(Y27) JIUQ-LC43-6032016 May 15.3898.0797.5770206286560.002232

DCZ-2D 2nd stage2016 29 B2016 May 15.113Cylinder10.9 longDecayed before being catalogued.

[NNA]< 1 day60503.35 dia

2016 May 15

Fragments2016 29 B-C2 pieces, both in orbitFor orbital information see extra pages at end of year

Galileo 14 (26B)2016 30 A2016 May 24.367Box +2 panels2.5 x 1.22016 May 24.1357.41858.952993223542235650.0004155

FM10 FM11 (Alizee)[41549]1 million years715x 1.12016 May 24.6057.43859.972995623554236000.0008231

[Soyuz 2-1BST-B/Fregat]KOU-ELS14.67 span2016 May 24.6157.43860.332996523552236200.001 231

(VS15)2016 May 24.8257.42859.082993623548235660.0003158

2016 May 29.6457.39845.502961923203232780.001295

2016 May 31.2457.40847.002965423272232790.00014

Galileo 13 (26A)2016 30 B2016 May 24.367Box +2 panels2.5 x 1.22016 May 24.1357.41859.882995423552235990.0008222

FM11 FM10 (Daniele)[41550]1 million years715x 1.12016 May 24.5957.41861.782999823555236840.002254

14.67 span2016 May 24.7557.41860.372996523554236200.001242

2016 May 25.3257.41860.252996223552236150.001232

2016 May 31.3257.41857.202989223457235690.002211

2016 Jun 4.4657.40856.902988523483235290.0008224

Fregat MT2016 30 C2016 May 24.367Spheres1.85 long2016 May 24.1357.41860.302996423554236160.001232

Upperstage[41551]+ nozzle3.38 dia2016 May 24.5857.42856.132986723417235600.00293

10502016 May 24.6057.42859.202993823545235740.0005178

2016 May 24.7557.41860.102995923553236080.0009236

2016 May 25.3257.42859.232993923515236060.002196

Thaicom 82016 31 A2016 May 27.902Box +2 panels??2016 May 27.9721.221947.9051666349902260.870180

[Falcon 9 FT] *[41552]> million years+3 reflectors? span 2016 May 28.0221.241946.8351647347901900.870180

(F9-25)CC-LC4030252.4+2.6 dia2016 May 30.676.952320.555806213074902920.665180

2.5x2.72016 Jun 3.351.423342.727405637805975500.403203

2016 Jun 6.600.311635.004597335887433030.081182

2016 Jun 7.660.241584.754502735878414180.062178

2016 Jun 7.720.131514.074367835885387130.032185

2016 Jun 8.790.031441.224226535881358920.0001215

2016 Jun 17.060.061440.024224135841358850.0005231

2016 Jun 23.030.031436.154216635781357940.0002133

2016 Jun 27.070.031435.434215235754357920.000596

2016 Jun 28.800.041436.054216435769358020.000448

2016 Jul 2.850.041436.104216535771358010.000443

Falcon 9 2nd stage2016 31 B2016 May 27.902Cylinder14.3 long2016 May 27.2621.211952.5851749349903920.870179

[41553]40003.66 dia2016 May 27.9721.121968.4852029374909270.870179

*Falcon 9 1st stage made a successful landing on the drone ship in the Atlantic Ocean.

Cosmos 25162016 32 A2016 May 29.364Cyl + box2.4 x 3.72016 May 29.5664.82676.072551719124191520.0005242

Glonass-M 53[41554]1 million years+2 panels7.2 span2016 Jun 3.5464.81673.422545018992191510.003230

[Soyuz 2-1B]PLE-LC43/41415

Fregat-M upperstage2016 32 B2016 May 29.364Spheres ring1.7 high2016 May 29.5864.80683.302569819148194910.00763

[41555]9603.35 dia2016 May 30.8664.79690.632588219182198240.01289

*Falcon 9 1st stage made a successful landing on the drone ship in the Atlantic Ocean.

Ziyuan 3-02 #12016 33 A2016 May 30.137Box +2 panels~4 high2016 May 30.2697.4994.4368704834990.001267

[CZ 4B][41556]2640x~2 x~2

WUZ-LC9~15 span

ÑuSat 1 #22016 33 B2016 May 30.137Box0.40x0.432016 May 30.2697.5094.4068684814990.001279

(Fresco)[41557]37x0.75

ÑuSat 2 #22016 33 C2016 May 30.137Box0.40x0.432016 May 30.2697.5094.4268694814990.001277

(Batata)[41558]37x0.75

DCZ 4B 3rd stage2016 33 D2016 May 30.137Cylinder4.92 long2016 May 30.2697.4092.1567582644950.0174

[41559]222.960 days17002.9 dia

2017 Jan 8.177

ÑuSat 1 fragment2016 33 E[43427]2018 Apr 17.8597.4997.5270194897910.02293

#1Chinese earth observation satellite.

#2 From Argentina for the Aleph-1 Earth Observation Constellation

Cosmos 2517 *2016 34 A2016 Jun 4.573Cylinder~4 long2016 Jun 4.6699.27104.0373279359630.002316

(GEO-IK 2-2)[41579]+2 panels1.3 dia2016 Jun 10.2899.28104.0373289379610.002300

[Rockot/Breeze-KM]PLE-LC133/3900

Breeze-KM stage2016 34 B2016 Jun 4.573Cyl+Cone2.6 long2016 Jun 4.7399.23101.0771876599580.021258

[41580]13202.5 dia

*Russian military spacecraft designed to map variations in Earth’s gravity field, rotation and tectonic movement. With a 1.2 dia radar antenna the sea

surface heights will be measured.

Intelsat 31 $2016 35 A2016 Jun 9.299Box +23 panels8.6 x 3.42016 Jun 10.5729.571356.43405913365650600.760180

[Proton-M/Breeze-M][41581]> million years6450x 3.12016 Jun 23.450.141435.074214535578359540.004358

BAI-LC81/2432.4 span

Breeze-M stage2016 35 B2016 Jun 9.299Cylinder2.61 long2016 Jun 10.5031.031284.83391501829637130.790183

[41582]23704.02.49 dia

Breeze-M tank2016 35 C2016 Jun 9.299Torus2.165 long2016 Jun 9.6150.76262.2813573359140300.504172

[41583]12904.1 dia

0.8 cross

#1Chinese earth observation satellite.

#2 From Argentina for the Aleph-1 Earth Observation Constellation

*Russian military spacecraft designed to map variations in Earth’s gravity field, rotation and tectonic movement. With a 1.2 dia radar antenna the sea

surface heights will be measured.

$Communication satellite with all KU-band channels leased to DirecTV Latin America, so also known as DLA-2.

USA 268 (NROL-37) *2016 36 A2016 Jun 11.744Box +2 panels?No TLE’s issued. Geosynchronous orbit. Orbits from amateur observations.

(Mentor 7)[41584]> million years+ dish2016 Jun 15.967.511437.184218635612360030.00541

[Delta IV Heavy]CC-LC37B6000?100 dia ?2016 Jun 23.947.511436.124216535597359760.00539

(Delta 374)2016 Jul 21.877.491436.124216535594359790.00548

Delta IV H 2nd stage2016 36 B2016 Jun 11.744Cylinder13.7 longNo TLE’s issued. Geosynchronous orbit.

(Delta CUS)[41585]34905 dia2016 Jul 24.247.611383.624113133865356400.022185

*Classified satellite believed to be Mentor 7, aka Advanced Orion.

Beidou-2 G7 (#23)2016 37 A2016 Jun 12.646Box +2 panels2.2 x 1.72016 Jun 12.8419.28608.0523775219345740.723179

[CZ-3C][41586]> million years>2000x 2.02016 Jun 23.521.841436.034216435776357940.0002258

XI-LC3

CZ-3C 3rd stage2016 37 B2016 Jun 12.646Cylinder12.38 long2016 Jun 12.8719.32630.0024344201357290.730180

[41587]27403.0 dia

ABS 2A $2016 38 A2016 Jun 15.603Box +2 panels4.5 x 2.12016 Jun 15.3224.691226.5337956398627570.821171