1982-101A
Two-tone telemetry; Hi res satellite
| Kosmos-1416 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1982 Oct 14 | 0910 | Launch by Soyuz-U | Baikonur |
| 0914 | Blok-I burn | ||
| 0918 | Blok-I sep | ||
| 1982 Oct 14 | 90.13 208x353x70.4 | ||
| 1982 Oct 14 | 90.18 209x358x70.4 | ||
| 1982 Oct 15 | 89.64 232x280 | ||
| 1982 Oct 28 | 89.43 225x267x70.4 | ||
| 1982 Oct 30 | |||
| 0640? | Deorbit | ||
| 0650? | PO sep | ||
| 0657? | Entry | ||
| 0712? | Landed | ||
1979-092A
Two-tone telemetry; Medium res satellite
| Kosmos-1142 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1979 Oct 22 | 1243 | Launch by Soyuz-U | Plesetsk |
| 1251 | Blok-I sep | ||
| 1979 Oct 22 | 90.34 198x382x72.87 | ||
| 1979 Oct 24 | 92.28 354x418x72.86 | ||
| 1979 Oct 28 | 353x417x72.9 | ||
| 1979 Nov 4 | |||
| 0712? | Deorbit | ||
| 0723? | PO sep | ||
| 0741? | Entry | ||
| 0753? | Landed | ||
1979-073A
Two-tone telemetry; Hi res satellite
| Kosmos-1120 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1979 Aug 11 | 0915 | Launch by Soyuz-U | Baikonur |
| 0919 | Blok-I burn | ||
| 0923 | Blok-I sep | ||
| 1979 Aug 11 | 89.81 169 x 360 x 70.6 | ||
| 1979 Aug 15 | 89.52 172 x 328 x 70.4 | ||
| 1979 Aug 20 | 89.34 170 x 313 x 70.4 | ||
| 1979 Aug 21 | 89.73 171 x 350 x 70.4 | ||
| 1979 Aug 23 | 89.66 170 x 344 x 70.4 | ||
| 1979 Aug 24 | |||
| 0605? | Deorbit | ||
| 0615? | PO sep | ||
| 0619? | Entry | ||
| 0635? | Landed | ||
1969-051A
The OGO F payload was launched at 1443 on 1969 Jun 5 by Thorad Agena D from Vandenberg and entered a 397 x 1089 km x 82.0 deg orbit. The 3-axis control failed on 1971 Jun 28 and the spacecraft was put on standby. It was turned on again from 1971 Oct 10 to 1972 Mar, and was finally decommissioned on 1972 Jul 14. It reentered on 1979 Oct 12.
| OGO 6 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1969 Jun 5 | 1442:45 | Launch by Thorad Agena D | |
| T+0:37 Castor burnout | |||
| T+1:42 Castor sep | |||
| T+3:38 Thor MECO | |||
| T+3:46 Thor VECO | |||
| 1446:38 | 3:53 Thor sep | -5675 x 322 x 79.89 | |
| 1447:30 | T+4:45 Agena MES-1 | ||
| T+4:54 Fairing sep | |||
| 1451:24 | T+8:39 Agena MECO | 397 x 1089 x 82.0 | |
| 1453:13 | T+10:28 Agena sep | ||
| 1969 Jul 25 | E-field antenna deployed | ||
| 1971 Jun 28 | 3-axis failed, on standby | ||
| 1971 Oct 10 | Recommissioned | ||
| 1972 Mar | On standby | ||
| 1972 Jul 14 | Decommissioned | ||
| 1979 Oct 12 | Reentered | ||
1969-016A
TOS G was the last of the Tiros I class TOS satellites, launched to back up ESSA VII, one of whose cameras had failed. Because of scheduling conflicts at Vandenberg it was launched from Cape Kennedy using a three stage Delta E1, requiring three dog-leg maneuvers during ascent to the polar sun-synchronous 1427 x 1508 km x 101.8 deg orbit. Launch was at 0747 on 1969 Feb 26 from Launch Complex 17 at Cape Kennedy and injection was south of Panama. ESSA IX transmitted until 1973 Nov 15.
| TOS G | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1969 Feb 26 | 0747:01 | Launch by Delta E1 | CK LC17B |
| Azimuth 140 deg | |||
| Castor I sep | |||
| 0749:31 | T+2:30 MECO | ||
| 0749 | St 1 sep | ||
| 0749 | SES S/N 20225, 6:11 | ||
| 0755 | SECO | ||
| St 2 sep | |||
| 0804? | TES FW-4D S/N 2322-1, burn time 32.2s | ||
| 0804? | TECO | ||
| 0805? | St 3 sep | 1427 x 1508 x 101.8 | |
| 1973 Nov 15 | end of tx | ||
