1976-010A
Intelsat 4A F2 was launched in Jan 1976 and became the AOR Primary Spare.
| Intelsat IVA F-2 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1976 Jan 29 | 2356 | Launch by Atlas Centaur | CC LC36 |
| 2358 | Booster sep | ||
| 1976 Jan 30 | 0000 | Atlas sep | |
| 0000:18? | MES-1 | ||
| 0000:30? | Fairing | ||
| 1976 Jan 30 | 0006:21? | T+10:21 Centaur MECO | 184? x 1800? x 28.1? |
| 0020:30? | MES-2 2:05 | ||
| 0022:35? | MECO-2 | ||
| 1976 Jan 30 | 0024 | Centaur sep, Orbit insertion | 578 x 36749 |
| Centaur venting | |||
| 0630? | Apo 1 | ||
| 1700? | Apo 2 | ||
| 1976 Jan 31
| 0300? | Apo 3 | |
| 1400? | Apo 4 | ||
| 1976 Feb 1 | 0019 | Apo 5, SVM-4A burn? | |
| 1976 Feb 1 | 0219 | Apo 5, SVM-4A burn, over W POR | |
1976 Feb 2 | GEO 140E +3E/d | ||
| 1420.2 35084 x 35869 x 0.11 (Fal) | |||
| 1976 Feb | AOR Primary Spare | GEO 29.5W | |
| 1977 Jan 21 | 1436.15 35779 x 35796 x 0.0 GEO 29.6W+0.0 | ||
| 1978 May 25 | 1436.07 35781 x 35791 x 0.0 GEO 29.5W | ||
| 1979 Jul 19 | 1436.11 35781 x 35792 x 0.0 GEO 29.5W+0.01W | ||
| 1979 Jul 21 | mv out | 1435.82 35766 x 35785 x 0.1 GEO 28.9W+0.06E | |
| 1979 Aug 14 | mv in | 1436.15 35779 x 35796 x 0.0 GEO 27.4W+0.02W | |
| 1979 Sep | Domestic Lease, contingency | GEO 27.5W | |
| 1980 Jan 14 | 1436.13 35774 x 35799 x 0.0 GEO 27.5W+0.02W | ||
| 1980 Oct 12 | 1436.10 35777 x 35795 x 0.0 GEO 27.4W+0.0W | ||
| 1980 Oct 22 | 1436.13 35777 x 35796 x 0.0 GEO 27.5W+0.02W | ||
| 1980 Nov? | Move to 21.5W | ||
| 1980 Dec 2 | 1436.17 35778 x 35798 x 0.0 GEO 21.7W+0.03W | ||
| 1981 Jan 2 | 1436.08 35776 x 35796 x 0.1 GEO 21.4W+0.0W | ||
| 1981 Jun 11 | AOR Major Path 2 | GEO 21.5W | |
| 1981 Oct 2 | 1436.15 35778 x 35796 x 0.3 GEO 21.5W+0.02W | ||
| 1982 Dec 18 | Domestic lease/contingency | 1436.13 35779 x 35794 x 0.0 GEO 21.5W | |
| 1983 Feb 21 | 1436.16 35783 x 35790 x 0.0 GEO 21.6W+0.01W | ||
| 1983 Feb 21 | mv out | ||
| 1983 Mar 30 | 1436.16 35775 x 35800 x 0.2 GEO 56.9E+0.02W | ||
| 1983 Apr | IOR domestic lease/contingency | GEO 57E | |
| 1983 Jun 1 | 1436.15 35774 x 35800 x 0.0 GEO 57.0E+0.02W | ||
| 1984 Jan 11 | 1436.10 35783 x 35790 x 0.1 GEO 56.9E+0.0W | ||
| 1984 Jan 17 | mv out | ||
| 1984 Mar 21 | 1438.08 35780 x 35870 x 0.3 GEO 46.8E+0.5W | ||
| 1984 Aug 4 | 1437.25 35751 x 35867 x 0.6 GEO 2.8W+0.3W | ||
| 1984 Aug | mv in, AOR Spare | GEO 4W | |
| 1984 Aug 17 | 1436.20 35749 x 35827 x 0.6 GEO 4.0W+0.03W | ||
| 1984 Oct 1 | 1436.14 35750 x 35825 x 0.8 GEO 4.9W+0.02W | ||
| 1985 Jan 13 | 1435.99 35759 x 35810 x 1.0 GEO 4.1W+0.02E | ||
| 1985 Mar 15 | 1435.91 35755 x 35810 x 1.2 GEO 1.5W+0.04E | ||
| 1985 Apr 13 | 1436.12 35761 x 35813 x 1.2 GEO 2.1W+0.01W | ||
| 1985 Nov 27 | 1436.05 35759 x 35812 x 1.8 GEO 1.9E+0.0E | ||
| 1985 Dec 19 | orbit raise | 1443.60 35910 x 35956 x 1.9 | |
| 1987 Mar 1 | 1444.43 35925 x 35973 x 3.0 | ||
| 1990 Nov 25 | 1444.41 35930 x 35967 x 6.5 | ||
| 1995 Nov 24 | 1444.57 35924 x 35980 x 10.3 | ||
| 1999 Apr 28 | 1444.42 35941 x 35957 x 11.9 | ||
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