2004-009A
GPS 2R-11 (SVN 59) was launched in 2004 to plane C, slot 3 to replace SVN 31, which had developed a suspect Navigation Data Unit.
Launch mass 2032 kg. Spin rate 55 rpm at launch injection.
| GPS 59 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2004 Mar 20 | 1753:00 | Launch by Delta 7925-9.5 | CC SLC17B |
| T+1:05 SRM 7-9 on | |||
| T+1:06 SRM 1-6 sep | |||
| T+2:11 SRM 7-9 sep | |||
| T+2:02 dog-leg 20s | |||
| T+4:23 MECO | |||
| T+4:31 St 1 sep | |||
| T+4:36 SES-1 | |||
| T+4:43 dog-leg 10s | |||
| T+4:58 Fairing sep | -3600 x 140? x 36.9 | ||
| 1803:44 | T+10:44 SECO-1 | 174.0 x 199.1 x 36.85 | |
| 1855:30 | T+1:02:30 SES-2 | ||
| 1856:10 | T+1:03:10 SECO-2 | 187 x 1152 x 37.20 | |
| T+1:04:00 Spinup | |||
| 1857:03 | T+1:04:03 St 2 sep | ||
| 1857:40 | T+1:04:40 TES | ||
| 1859:07 | T+1:06:07 TECO | ||
| T+1:06:50 Third stage NCS (nutation thruster) blowdown | |||
| T+1:07:43 end NCS blowdown | |||
| 1901:00 | T+1:08:00 St 3 sep | ||
| 1901:02 | T+1:08:02 St 3 yo deploy | ||
| 1939 | T+1:46:40 SES-3 | ||
| 1940 | T+1:47:07 SECO-3 depletion | ||
| 2004 Mar 20 | 355.69 183 x 20318 x 38.9 | ||
| 2004 Mar 23 | 0256? | AKM burn over 62E 7S | |
| 2004 Mar 28 | 718.02 20089 x 20276 x 55.1 | ||
