1977-003A
Low res photo recon satellite. PDM telemetry, extended duration.
| Kosmos-889 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1977 Jan 20 | 0830 | Launch by Soyuz-U | Baikonur |
| 0834 | Blok-I burn | ||
| 0838 | Blok-I sep | ||
| 1977 Jan 21 | 89.81 201 x 328 x 71.4 | ||
| 1977 Feb 1 | 89.71 199 x 320 x 71.4 | ||
| 1977 Feb 1 | |||
| 0610? | Deorbit | ||
| 0620? | PO sep | ||
| 0626? | Entry | ||
| 0640? | Landed | ||
1987-102A
| Kosmos-1901 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1987 Dec 14 | 1129 | Launch by Soyuz | KB |
| 1133? | Blok-A sep | ||
| 1138? | Blok-I sep | ||
| 1987 Dec 14 | 89.79 174 x 353 x 64.9 | ||
| 1987 Dec 18 | 89.58 171 x 336 x 64.9 | ||
| 1987 Dec 20 | 89.47 169 x 327 x 64.9 | ||
| 1987 Dec 21 | 89.55 174 x 330 x 64.9 | ||
| 1987 Dec 25 | 89.28 169 x 308 x 64.9 | ||
| 1987 Dec 26 | 89.39 170 x 318 x 64.9 | ||
| 1987 Dec 29 | 89.17 167 x 299 x 64.9 | ||
| 1987 Dec 30 | 89.73 174 x 347 x 64.9 | ||
| 1987 Dec 31 | SpK-1 fiducial | ||
| 1988 Jan 5 | 89.39 169 x 319 x 64.9 | ||
| 1988 Jan 12 | 89.45 167 x 326 x 64.9 | ||
| 1988 Jan 13 | 90.14 171 x 391 x 64.9 | ||
| 1988 Jan 16 | SpK-2 fiducial | ||
| 1988 Jan 20 | 89.04 166 x 287 x 64.9 | ||
| 1988 Jan 21 | 89.58 168 x 339 x 64.9 | ||
| 1988 Jan 24 | 89.33 165 x 316 x 64.9 | ||
| 1988 Feb 1 | 89.17 168 x 298 x 64.9 | ||
| 1988 Feb 3 | |||
| 2037? | Deorbit | ||
| 2054? | Entry | ||
| 2103? | Landed | ||
1989-055A
Resurs F-1 14F43 No. 47 was launched on 1989 Jul 18 and announced as the third Resurs F. It carried out a 22 day extended duration flight and released two Pion subsatellites.
| Resurs F-1 14F43 No. 47 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1989 Jul 18 | 0945 | Launch by Soyuz-U | PL LC16 |
| 0953 | Blok-I sep | 88.57 183 x 223 x 82.6 | |
| 1989 Jul 19 | 88.6 182 x 225 x 82.5 | ||
| Orbit raise | 89.86 260 x 274 x 82.6 | ||
| 1989 Jul 24 | 89.82 258 x 272 x 82.6 | ||
| 1989 Jul 26 | 89.80 257 x 271 x 82.6 | ||
| Orbit trim | 89.86 260 x 275 x 82.6 | ||
| 1989 Jul 31 | 89.84 258 x 273 x 82.6 | ||
| 1989 Aug 1 | 1700 | Orbit trim | 89.86 259 x 275 x 82.6 |
| 1989 Aug 5 | 2200 | 89.78 255 x 272 x 82.6 | |
| 1989 Aug 7 | Pion-3 released | ||
| Pion-4 released | |||
| 1989 Aug 9 | |||
| 0528? | Deorbit | ||
| 0536? | PO sep | ||
| 0545? | Entry | ||
| 0607? | Landed | ||
1975-088A
Kosmos-769 flew a 12 day mission and carried an FEU-170 SpK recovery capsule test.
| Kosmos-769 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1975 Sep 23 | 1000 | Launch by Soyuz-U | Plesetsk |
| 1004 | Blok-I burn | ||
| 1008 | Blok-I sep | ||
| 1975 Sep 23 | 89.59 202 x 305 x 72.8 | ||
| 1975 Oct 1 | FEU-170 sep | ||
| 0558? | Deorbit | ||
| 0608? | Entry | ||
| 0620? | Landed | ||
| 1975 Oct 4 | 89.50 200 x 298 x 72.8 | ||
| 1975 Oct 5 | |||
| 0353? | Deorbit | ||
| 0403? | PO sep | ||
| 0410? | Entry | ||
| 0422? | Landed | ||
1969-096A
Kosmos-308 was the last of the low apogee subgroup of DS-P1-I missions.
| Kosmos-308 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1969 Nov 4 | 1200 | Launch by 11K63 | PL |
| 1202 | Stage 2 burn | ||
| 1207 | Stage 2 sep | ||
| 1969 Nov 5 | 0500 | 91.34 271 x 408 x 71.02 | |
| 1969 Dec 6 | 2025? | Stage 2 reentered | |
| 1970 Jan 4 | 1144? | Reentered | |
1973-094A
DS-P1-Yu No. 64 was launched in Nov 1973, the second such launch in a week.
| Kosmos-611 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1973 Nov 28 | 0930 | Launch by 11K63 | NIIP-53 LC133/1 |
| 0932 | Stage 2 burn | ||
| 0936? | Stage 2 sep | ||
| 92.1 270 x 481 x 71.0 | |||
| 1974 Apr? | End of ops | ||
| 1974 Jun 19 | Reentered | ||
1973-039A
Because of the problem of terrestrial radio interference, the second RAE, RAE B, was designed to make its observations in lunar orbit, shielded from Earth while it skimmed above the lunar farside. The spacecraft had a velocity control thruster to refine the lunar orbit.
RAE 2 (Explorer 49) was launched at 1413 on 1973 Jun 10 by a Delta 1913 from Cape Kennedy. The Delta stage ignited at 1417:30 and cut off at 1422:30 to place the combination in parking orbit. At 1425 the Delta reignited for 29s to enter a 107.8 min, 182 x 2074 km x 29.3 deg orbit. At 1428 the Star 37D third stage ignited for the 44s translunar injection burn, entering a 182 x 390244 km x 29.1 deg orbit. RAE 2 separated from the Star 37D at 1430. The VCS was used to make a midcourse correction at 1528 on Jun 11. The TE-M-479 (Star 17) solid motor fired at 0721 on Jun 15 to insert RAE 2 in a 241 min, 1123 x 1334 km x 38.3 deg lunar orbit. The Star 17 was jettisoned on Jun 18, and the same day the VCS fired to lower the orbit to 221.2 min, 1053 x 1064 km x 38.7 deg. The 37m dipole antenna was extended on Jun 20.
Another object was cataloged in lunar orbit, probably implying the VCS was also ejected after use.
It was reported in Jun 1973 that on Jul 4 the dipole would be retracted, the VCS used to adjust the orbit, and the two main V antennas would be deployed first to 183m, and then a week later to 229m. Total span is 400m. RAE also has a 190m stabilization boom.
RAE 2 operated in lunar orbit until 1977 Apr 30. After that, engineers performed end-of-life tests retracting and extending the antennas. It probably impacted the lunar surface later in 1977. Orbit according to an internal document was 1058 x 1070 km x 59 deg with a 222 min period; this is presumably the first orbit after VCS sep.
| Explorer 49 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1973 Jun 10 | 1413:00 | Launch by Delta 1913 | CK LC17B |
| T+0:38 SRM 4-9 burnout | |||
| T+0:39 SRM 1-3 on | |||
| T+1:17 SRM 1-3 out | |||
| T+1:25 SRM 1-9 sep | |||
| T+4:29 MECO | |||
| T+4:33 VECO | |||
| T+4:36 St 1 sep | |||
| 1417:41 | T+4:41 SES-1 | ||
| T+4:55 Fairing sep | |||
| 1422:31 | T+9:31 SECO-1 | ||
| 1425:57 | T+13:57 SES-2 29s | ||
| 1426:28 | T+14:28 SECO-2 | 182 x 2074 x 29.3 | |
| T+15:02 Spinup | |||
| 1428:05 | T+15:05 Stage 2 sep | ||
| 1428:19 | T+15:17.9 Star 37D burn 44s | ||
| 1429:03 | T+16:02.7 Star 37D burnout | ||
| 1430:43 | T+17:43 Star 37D separation | 182 x 390244 x 29.1 | |
| 1430:45 | T+17:45 Star 37D release yo weight | ||
| 1973 Jun 11 | 0600? | Pass EL1:4 | |
| 1973 Jun 11 | 1528 | VCPS TCM | |
| 1973 Jun 13 | 0600? | Enter lunar sphere | |
| 1973 Jun 15 | 0721 | Star 17 burn 22s LOI | 241.0 1123 x 1334 x 61.4 |
| 1973 Jun 18 | 0725? | Star 17 sep | |
| Despin to 12 rpm (ACS) | |||
| VCPS lower orbit to avoid LIM | 221.2 1053 x 1064 x 61.4 | ||
| 1973 Jun 20 | 37m dipole extended | ||
| 1973 Jul 4 | Retract dipole? | ||
| 1973 Jul 9 | Final orbit trim | ||
| 1973 Jul 9? | VCPS separated | ||
| 1973 Jul | Deploy libration damper | ||
| 1973 Jul 12 | Deploy to 183m | ||
| Experiment turn on | |||
| 1973 Jul 29 | Begin first lunar shadow period | ||
| 1973 Oct 26 | End first shadow period | ||
| 1973 Nov 8 | Upper V extension to 200m | ||
| 1973 Nov 14 | Upper V deploy to 229m | ||
| 1974 Jan 3 | Begin second lunar shadow period | ||
| 1974 Jan 31 | 222.0 1059 x 1071 x 62.0 | ||
| 1974 Mar 22 | End second shadow period | ||
| 1974 Jun 10 | Begin third shadow period | ||
| 1974 Aug 28 | End third shadow period | ||
| 1974 Oct 11 | One lower-V boom extended to 229m | ||
| 1974 Nov 6 | Second lower-V boom extended to 229m | ||
| 1974 Nov 17 | Fourth shadow period | ||
| 1975 Feb 1 | End shadow period 4 | ||
| 1975 Apr 21 | Shadow period 5 | ||
| 1975 Jul 1 | Begin new-moon-intensive 50-percent data coverage | ||
| 1975 Jul 9 | End shadow period 5 | ||
| 1975 Dec 24 | Resume full time coverage | ||
| 1976 Apr 17 | Reduce to 50 percent coverage again | ||
| 1976 Oct 19 | Resume full time coverage | ||
| 1977 Apr 30 | End of ops | ||
1977-109A
| Kosmos-963 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1977 Nov 24 | 1430 | Launch by 11K65M | PL |
| 1432 | Stage 2 burn | ||
| 1438? | Stage 2 MECO | ||
| 1533? | Stage 2 restart | ||
| 1533? | Stage 2 sep | ||
| 1977 Nov 24 | 109.4 1182x1210x82.9 | ||
1963-049B
Transit VBN-2 was launched on 1963 Dec 5, and successfully stabilized itself. On Dec 16 optical confirmation was obtained that the boom had extended. On Dec 22 it began tumbling, but a magnetic damping system successfully restored stability by 1964 Jan 23 and it went into use as the first operational navigation satellite the following day.
| Transit VBN-2 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1963 Dec 5 | 2151 | Launch by Thor Ablestar | V 75-1-1 |
| 2153 | Thor MECO (T+2:25) | ||
| 2153 | AB start (T+2:28) | ||
| 2153 | Thor sep (T+2:29) | ||
| 2153 | Thor VECO (T+2:38) | ||
| 2158 | AB MECO (T+7:29) | ||
| 2229 | AB burn 2 (T+38:44) | ||
| 2229 | AB MECO (T+38:51) | ||
| 2231 | AB sep (T+40:32) | 107.0 1063 x 1113 x 89.96 (VCR) | |
| 1067 x 1112 x 89.98 (RAE) | |||
| Gravity gradient boom extended | |||
| Stablized | |||
| 1963 Dec 22 | Tumbling, begin damping | ||
| 1964 Jan 23 | Damping completed | ||
| 1964 Jan 24 | In operation | ||
| 1964 Nov 1 | End of operations | ||
| 1970 May | Under APL control for testing | ||
1961-S357
The first Saturn C-1 launch, Saturn 101 or SA-1, took place from Launch Complex 34 at Cape Canaveral at 1506 on 1961 Oct 27. The Saturn S-4-1 and S-V-1 upper stages were both dummies. The Centaur was topped by a payload adapter, a Jupiter aft unit (truncated cone) and a Jupiter nosecone. Apogee was 136 km.
SP-4205 gives 1800:06 as the launch time, but the postlaunch report MPR-SAT-WF-61-8 gives 1506:03 and seems definitive (consistent with other times given in same document, so not a typo).
Mass was 153421 kg at OECO including 86874 kg of water ballast.
| SA-1 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1961 Oct 27 | 1506:03 | Launch by Saturn C-1 | |
| 1507:53 | T+1:50 IECO | ||
| 1507:59 | T+1:56 OECO | ||
| 1508:02 | T+1:59 end of thrust decay | ||
| 1510:12 | T+4:09 Apogee 136 km | -6330 x 136 | |
| 1512:52 | T+6:49 LOS at 19 km descending | ||
1985-048A
Mission 51-G deployed three PAM-D class satellites and carried out the first Spartan free-flyer mission.
| STS 51-G mission events | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1985 May 28 | Roll to VAB | ||
| 1985 Jun 4 | Rollout | LC39A | |
| 1985 Jun 17 | 1133:00 | Launch from LC39A | |
| 1135:05 | SRB sep, 50.0 km | ||
| 1141:36 | MECO | ||
| 1141:54 | ET sep, 112.2 km | 88.53 61 x 343 x 28.5 | |
| 88.73 68 x 355 x 28.5 (OMS dV) | |||
| 1213:29 | OMS-2 2:58 85m/s | ||
| 1216:27 | OMS-2 CO | ||
| 1259 | PLBD open | 91.65 352 x 358 x 28.5 | |
| 1937:51 | Morelos deploy | ||
| 1953 | SEP-1 (OMS LH 13s) 3m/s | 91.78 354 x 368 x 28.47 | |
| 1985 Jun 18 | 1356:56 | Arabsat deploy | |
| 1412? | SEP-2 (OMS LH 13s) 3m/s | 91.90 354 x 380 x 28.47 | |
| 1985 Jun 19 | 1120:36 | Telstar deploy | |
| 1135? | SEP-3 (OMS LH 13s) 3m/s | 92.01 355 x 391 x 28.5 | |
| 1985 Jun 20 | 1445? | RMS grapple Spartan | |
| 1507 | RMS unberth Spartan | ||
| 1602:39 | RMS deploy Spartan | ||
| 1605 | RCS sep 1 | ||
| 1625 | RCS sep 2 | 92.03 356 x 391 x 28.5 | |
| 1985 Jun 21 | 0829 | 92.03 355 x 392 x 28.5 | |
| 1654 | NC-1 (RCS), range 170km | 91.98 352 x 389 x 28.5 | |
| 1985 Jun 22 | 0814 | NC-2 (RCS), range 65 km | |
| 0842 | Tally ho Spartan | ||
| 1020 | NCC (RCS) out of plane | 91.95 350 x 389 x 28.5 | |
| 1118 | TI (RCS) 15 km range | ||
| 1310 | At 6m/s, approaching Spartan | ||
| 1323 | Rendezvous with Spartan | ||
| 1331:55 | RMS grapple Spartan | 91.96 352 x 388 x 28.5 | |
| 1422? | Berth Spartan | ||
| 1618 | OMS-6 (RH 111s) 30m/s | 90.92 284 x 354 x 28.5 | |
| 1985 Jun 24 | 0837 | Go for PLBD close | |
| 0856 | PLBD closed | 90.91 284 x 354 x 28.5 | |
| 1207:30 | OMS DO (150s) 85m/s | ||
| 1210:01 | OMS DO CO | ||
| 1241:22 | Entry | ||
| 1311:52 | Landed RW23 EAFB | ||
| 1312:05 | NGTD | ||
| 1312:24 | Wheels stop | ||
| 1985 Jun 28 | 1310 | SCA takeoff | EAFB |
| 1503 | SCA landing | Bergstrom AFB TX | |
| 1748 | SCA takeoff | Bergstrom AFB TX | |
| 2052 | SCA landing | KSC SLF | |
| 1985 Jun 29 | 0030 | Tow to OPF | |
1986-082A
Raduga No. 30 (Gran' 11F638 No. 30) was launched in Oct 1986. It was stationed at 45E until 1991, and then at 35E until it was decommissioned in 1993.
| Raduga No. 30(F20) | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1986 Oct 25 | 1543 | Launch by Proton-K | KB |
| 1552 | Stage 3 sep | 181 x 181 x 51.6 | |
| 1700? | DM burn 1 | ||
| 335 x 36681 x 47.4 | |||
| 2216? | DM burn 2 | ||
| 2220? | DM sep | ||
| 1986 Oct 27 | 1476.87 36538 x 36623 x 1.3 GEO 69.3E+9.9W | ||
| 1986 Oct 31 | 1436.97 35757 x 35849 x 1.3 GEO 45.1E+0.2W | ||
| 1986 Nov 7 | mv in | 1436.10 35750 x 35822 x 1.3 GEO 44.7E | |
| 1986 Dec 18 | 1435.86 35741 x 35822 x 1.2 GEO 45.7E | ||
| 1987 Apr 13 | 1436.30 35783 x 35797 x 0.9 GEO 45.0E | ||
| 1988 Mar 6 | 1435.99 35774 x 35794 x 0.1 GEO 44.2E | ||
| 1989 Sep 6 | 1436.17 35786 x 35789 x 1.4 GEO 44.3E | ||
| 1991 Jan 23 | 1436.29 35782 x 35798 x 2.7 GEO 45.0E | ||
| 1991 Aug 7 | 1436.19 35786 x 35790 x 3.1 GEO 44.3E | ||
| 1991 Aug 11 | mv out | 1441.44 35793 x 35988 x 3.1 | |
| 1991 Aug 14 | mv in | 1436.21 35784 x 35793 x 3.1 GEO 34.9E | |
| 1991 Oct 28 | 1436.10 35767 x 35805 x 3.3 GEO 34.5E | ||
| 1992 Jul 21 | 1435.92 35773 x 35792 x 4.0 GEO 34.9E | ||
| 1993 Apr 16 | 1435.92 35773 x 35793 x 4.6 GEO 34.5E | ||
| 1993 Sep 30 | 1436.00 35779 x 35789 x 4.9 GEO 34.4E | ||
1972-102A
Kosmos-539 was launched in Dec 1972. It was the first of a series of Sfera satellites to enter a higher orbit with a period of 114 minutes.
| Kosmos-539 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1972 Dec 21 | 0205 | Launch by 11K65M | PL |
| 0207 | Stage 2 burn | ||
| 0213? | Stage 2 coast | ||
| 0258? | Stage 2 burn 2 | ||
| 0258? | Stage 2 sep | ||
| 1972 Dec 28 | 0230 | 112.98 1343 x 1383 x 74.0 | |
1983-092A
This flight saw the single use of a TC beacon in the Zenit program.
| Kosmos-1495 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1983 Sep 3 | 1015 | Launch by Soyuz | Plesetsk |
| 1019 | Blok-I burn | ||
| 1023 | Blok-I sep | ||
| 1983 Sep 3 | 88.83 208 x 224 x 82.3 | ||
| 1983 Sep 4 | 88.82 207 x 224 x 82.3 | ||
| 1983 Sep 4 | Raise orbit | 88.98 213 x 235 x 82.3 | |
| 1983 Sep 12 | 88.84 207 x 226 x 82.3 | ||
| 1983 Sep 13 | Raise orbit | 88.98 214 x 232 x 82.3 | |
| 1983 Sep 15 | 88.93 213 x 229 x 82.3 | ||
| 1983 Sep 16 | |||
| 0626? | Deorbit | ||
| 0635? | PO sep | ||
| 0642? | Entry | ||
| 0702? | Landed | ||
1980-103A
Prognoz-8 was launched in Dec 1980 and continued the space science investigations of its predecessors.
| Prognoz-8 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1980 Dec 25 | 0402 | Launch by Molniya-M | KB |
| 0411 | Blok-I MECO | ||
| 0411 | Blok I sep | ||
| 0507? | Blok-L burn | ||
| 0511? | Blok-L MECO | ||
| 0511? | Blok-L sep | ||
| 2354 | Pass EL1:4 | ||
| 5689.0 980 x 197390 x 65.8 | |||
| 1981 Sep | Still operating | ||
| 1981 Oct 10 | end of ops | ||
| 1984 Dec 28 | reentered | ||
1974-064A
The second 7K-TM test flight was 11F615A12 No. 72, a 6 day mission in Aug 1974.
| Kosmos-672 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1974 Aug 12 | 0625:02 | Launch by Soyuz | KB |
| 0627 | Blok BVGD sep | ||
| 0629 | Blok A sep | ||
| 0633 | Blok I MECO | ||
| 0633 | Blok-I sep | ||
| 1974 Aug 12 | 1041 | 89.51 195 x 304 x 51.8 | |
| 1208 | 88.65 194 x 220 x 51.8 | ||
| 1974 Aug 13 | 0720 | 88.65 193 x 222 x 51.8 | |
| Raise perigee | |||
| 1974 Aug 14 | 0702 | 88.96 223 x 223 x 51.8 | |
| Orbit adjust | |||
| 1974 Aug 14 | 1259 | 89.13 226 x 236 x 51.8 | |
| 1974 Aug 16 | 1356 | 89.02 223 x 228 x 51.8 | |
| 1974 Aug 17 | 0743 | 88.95 219 x 225 x 51.8 | |
| 1974 Aug 17 | 2103 | 88.92 218 x 223 x 51.8 | |
| 1974 Aug 18 | 0420? | Deorbit | |
| 0423? | DO CO | ||
| 0436? | Modules sep | ||
| 0441? | Entry | -173? x 223 x 51.8 | |
| 0505 | Landed | ||
1962-043A
The second 2MV-1 probe suffered a similar fate to the first, reentering from parking orbit after 5 days. A fuel valve on the S1.5400A1 engine failed to open and the Blok-L main engine did not ignite.
| 2MV-1 No. 2 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1962 Sep 1 | 0212:30 | Launch by 8K78 | KB |
| 0217 | Blok-A sep | ||
| 0217 | Blok-I burn | ||
| 0221 | Blok-I sep | 180 x 310 x 64.9 | |
| 0312 | BOZ burn | ||
| 0314:00 | Blok-L failed to ignite | ||
| 1962 Sep 6 | Reentered | ||
1966-083A
KH-7 32 was launched on 1966 Sep 16 by Atlas Agena D from Vandenberg on a 6 day mission. The Agena D rocket reentered after 1 day; shortly after orbit insertion a small piggyback satellite was launched from the Agena aft rack. This was the last KH-7 to carry such a subsatellite. As well as the OCV, the Agena, and the subsatellite, one debris object was tracked; the SATCAT and the UN give a 474 x 498 km x 94.0 deg orbit and a decay date of Oct 30, so it was probably a small sensor cover from the subsatellite.
| KH-7 32 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1966 Sep 16 | 1759 | Launch by Atlas Agena D | V |
| T+2:18? BECO | |||
| T+4:37? SECO | |||
| T+4:54? VECO | |||
| T+4:59? Atlas sep | |||
| T+5:51? Agena MES | |||
| 1808 | T+9:50? Agena MECO | ||
| 1966 Sep 16 | 1935? | Subsatellite ejected from Agena | |
| 1966 Sep 16 | OCV separated from Agena | ||
| 1966 Sep 17 | 89.4 148 x 333 x 94.0 (RAE) | ||
| 1966 Sep 23 | Rev 111 last image | ||
| 1966 Sep 23 | SRV recovered | ||
| 2247 | Rev 111 deorbit opp | ||
| 1966 Sep 25 | reentered | ||
