1989-013A
The first Block II GPS satellite was SVN 14 (PRN 14, USA 35). It used the first Delta 6925 (Interim Delta II) launch vehicle, and was the first GPS launch from Cape Canaveral. Navstar 14 entered the E plane (slot E1)
| Navstar 14 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1989 Feb 14 | 1830 | Launch by Delta II 6925 | CC LC17 |
| T+0:56 SRM 1-3,7-9 out | |||
| T+1:01 SRM 4-6 on | |||
| T+1:02 SRM 1-3 sep | |||
| T+1:03 SRM 7-9 sep | |||
| T+1:57 SRM 4-6 off | |||
| T+2:02 SRM 4-6 sep | |||
| T+4:25 MECO | |||
| T+4:31 VECO | |||
| T+4:33 Stage 1 sep | |||
| 1834 | Stage 2 TIG (T+4:38) | ||
| 1834 | Fairing sep (T+4:50) | ||
| 1841 | SECO-1 Stage 2 cutoff (T+11:37) | 166 x 200 x 35.66 | |
| T+20:55 spinup | |||
| 1850 | T+20:58 Delta sep | ||
| T+21:35 TES | |||
| 1853 | T+23:02 TECO | ||
| 1854 | T+24:55 Stage 3 sep | 358.66 157 x 20531 x 37.4 | |
| 1854 | T+24:57 Yo weight | ||
| T+1:05:00 SES-2 depletion | |||
| 1936 | T+1:06:20 SECO-2 depletion | 95.21 186 x 872 x 30.3 (B) | |
| 1989 Feb 16 | 1530? | Star 37 apogee burn | 720.01 20010 x 20455 x 55.1 |
| 1989 Feb 18 | 715.02 19870 x 20349 x 55.1 | ||
| 1989 Apr 15 | In service | ||
| 1997 Feb 1 | Operating in slot E1 | ||
| 2000 Mar 26 | Reaction wheel failure | ||
| 2000 Jun 14 | Decommissioned | ||
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