Orbital elements of DELTA 4 R/B
| Launched | 5 December 2009 |
| Flight ended | – |
| Launch site | Air Force Eastern Test Range, Florida, USA |
| Owner | United States |
| NORAD ID | 36109 |
| Date fetched |
Epoch osculation |
Inc. [°] |
Ecc. | RA asc node [hr] |
Arg Peri. [°] |
Mean anom [°] |
Mean motion [rev/day] |
Abs. mag |
| Date fetched |
Epoch osculation |
Inc. [°] |
Ecc. | RA asc node [hr] |
Arg Peri. [°] |
Mean anom [°] |
Mean motion [rev/day] |
Abs. mag |
| 2025 Nov 26 18:57 | 2025 Nov 25 04:03:20 | 25.4242 | 0.81620 | 22.0413 | 138.8997 | 356.6105 | 1.19252 | 3.500 |
| 2025 Nov 25 18:57 | 2025 Nov 25 04:03:20 | 25.4242 | 0.81620 | 22.0413 | 138.8997 | 356.6105 | 1.19252 | 3.500 |
| 2025 Nov 24 18:56 | 2025 Nov 20 01:37:45 | 25.4444 | 0.81610 | 22.0943 | 137.5031 | 356.6105 | 1.19252 | 3.500 |
| 2025 Nov 23 18:57 | 2025 Nov 20 01:37:45 | 25.4444 | 0.81610 | 22.0943 | 137.5031 | 356.6105 | 1.19252 | 3.500 |
| 2025 Nov 21 18:57 | 2025 Nov 20 01:37:45 | 25.4444 | 0.81610 | 22.0943 | 137.5031 | 356.6105 | 1.19252 | 3.500 |
| 2025 Nov 20 18:56 | 2025 Nov 20 01:37:45 | 25.4444 | 0.81610 | 22.0943 | 137.5031 | 356.6105 | 1.19252 | 3.500 |
| 2025 Nov 18 18:57 | 2025 Nov 08 08:12:47 | 25.4877 | 0.81593 | 22.2153 | 134.3160 | 356.6105 | 1.19252 | 3.500 |
| 2025 Nov 16 18:58 | 2025 Nov 08 08:12:47 | 25.4877 | 0.81593 | 22.2153 | 134.3160 | 356.6105 | 1.19252 | 3.500 |
| 2025 Nov 15 18:57 | 2025 Nov 08 08:12:47 | 25.4877 | 0.81593 | 22.2153 | 134.3160 | 356.6105 | 1.19252 | 3.500 |
| 2025 Nov 13 18:56 | 2025 Nov 08 08:12:47 | 25.4877 | 0.81593 | 22.2153 | 134.3160 | 356.6105 | 1.19252 | 3.500 |
| 2025 Nov 12 18:57 | 2025 Nov 08 08:12:47 | 25.4877 | 0.81593 | 22.2153 | 134.3160 | 356.6105 | 1.19252 | 3.500 |
| 2025 Nov 11 18:55 | 2025 Nov 08 08:12:47 | 25.4877 | 0.81593 | 22.2153 | 134.3160 | 356.6105 | 1.19252 | 3.500 |
| 2025 Nov 10 18:57 | 2025 Nov 08 08:12:47 | 25.4877 | 0.81593 | 22.2153 | 134.3160 | 356.6105 | 1.19252 | 3.500 |
| 2025 Nov 09 18:57 | 2025 Nov 08 08:12:47 | 25.4877 | 0.81593 | 22.2153 | 134.3160 | 356.6105 | 1.19252 | 3.500 |
| 2025 Nov 08 18:56 | 2025 Nov 01 14:52:31 | 25.5074 | 0.81582 | 22.2845 | 132.4989 | 356.6105 | 1.19252 | 3.500 |
| 2025 Nov 07 18:57 | 2025 Nov 01 14:52:31 | 25.5074 | 0.81582 | 22.2845 | 132.4989 | 356.6105 | 1.19252 | 3.500 |
| 2025 Nov 05 18:57 | 2025 Nov 01 14:52:31 | 25.5074 | 0.81582 | 22.2845 | 132.4989 | 356.6105 | 1.19252 | 3.500 |
| 2025 Nov 04 18:57 | 2025 Nov 01 14:52:31 | 25.5074 | 0.81582 | 22.2845 | 132.4989 | 356.6105 | 1.19252 | 3.500 |
| 2025 Nov 03 18:57 | 2025 Nov 01 14:52:31 | 25.5074 | 0.81582 | 22.2845 | 132.4989 | 356.6105 | 1.19252 | 3.500 |
| 2025 Nov 02 18:57 | 2025 Oct 29 08:08:34 | 25.5154 | 0.81579 | 22.3184 | 131.6128 | 356.6105 | 1.19252 | 3.500 |
| 2025 Nov 01 18:58 | 2025 Oct 29 08:08:34 | 25.5154 | 0.81579 | 22.3184 | 131.6128 | 356.6105 | 1.19252 | 3.500 |
| 2025 Oct 31 18:57 | 2025 Oct 29 08:08:34 | 25.5154 | 0.81579 | 22.3184 | 131.6128 | 356.6105 | 1.19252 | 3.500 |
| 2025 Oct 30 18:57 | 2025 Oct 29 08:08:34 | 25.5154 | 0.81579 | 22.3184 | 131.6128 | 356.6105 | 1.19252 | 3.500 |