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 05 18:57 | 2025 Nov 01 14:52:31 | 25.5074 | 0.81582 | 22.2845 | 132.4989 | 327.0990 | 1.19252 | 3.500 |
| 2025 Nov 04 18:57 | 2025 Nov 01 14:52:31 | 25.5074 | 0.81582 | 22.2845 | 132.4989 | 327.0990 | 1.19252 | 3.500 |
| 2025 Nov 03 18:57 | 2025 Nov 01 14:52:31 | 25.5074 | 0.81582 | 22.2845 | 132.4989 | 327.0990 | 1.19252 | 3.500 |
| 2025 Nov 02 18:57 | 2025 Oct 29 08:08:34 | 25.5154 | 0.81579 | 22.3184 | 131.6128 | 327.0990 | 1.19252 | 3.500 |
| 2025 Nov 01 18:58 | 2025 Oct 29 08:08:34 | 25.5154 | 0.81579 | 22.3184 | 131.6128 | 327.0990 | 1.19252 | 3.500 |
| 2025 Oct 31 18:57 | 2025 Oct 29 08:08:34 | 25.5154 | 0.81579 | 22.3184 | 131.6128 | 327.0990 | 1.19252 | 3.500 |
| 2025 Oct 30 18:57 | 2025 Oct 29 08:08:34 | 25.5154 | 0.81579 | 22.3184 | 131.6128 | 327.0990 | 1.19252 | 3.500 |
| 2025 Oct 29 18:57 | 2025 Oct 29 08:08:34 | 25.5154 | 0.81579 | 22.3184 | 131.6128 | 327.0990 | 1.19252 | 3.500 |
| 2025 Oct 28 18:57 | 2025 Oct 23 11:19:12 | 25.5297 | 0.81571 | 22.3788 | 130.0298 | 327.0990 | 1.19252 | 3.500 |
| 2025 Oct 27 18:57 | 2025 Oct 23 11:19:12 | 25.5297 | 0.81571 | 22.3788 | 130.0298 | 327.0990 | 1.19252 | 3.500 |
| 2025 Oct 26 18:57 | 2025 Oct 23 11:19:12 | 25.5297 | 0.81571 | 22.3788 | 130.0298 | 327.0990 | 1.19252 | 3.500 |
| 2025 Oct 25 17:57 | 2025 Oct 23 11:19:12 | 25.5297 | 0.81571 | 22.3788 | 130.0298 | 327.0990 | 1.19252 | 3.500 |
| 2025 Oct 24 17:57 | 2025 Oct 23 11:19:12 | 25.5297 | 0.81571 | 22.3788 | 130.0298 | 327.0990 | 1.19252 | 3.500 |
| 2025 Oct 22 17:56 | 2025 Oct 17 12:46:52 | 25.5435 | 0.81567 | 22.4397 | 128.4327 | 327.0990 | 1.19252 | 3.500 |
| 2025 Oct 21 17:56 | 2025 Oct 17 12:46:52 | 25.5435 | 0.81567 | 22.4397 | 128.4327 | 327.0990 | 1.19252 | 3.500 |
| 2025 Oct 20 17:56 | 2025 Oct 17 12:46:52 | 25.5435 | 0.81567 | 22.4397 | 128.4327 | 327.0990 | 1.19252 | 3.500 |
| 2025 Oct 19 17:56 | 2025 Oct 17 12:46:52 | 25.5435 | 0.81567 | 22.4397 | 128.4327 | 327.0990 | 1.19252 | 3.500 |
| 2025 Oct 18 17:56 | 2025 Oct 17 12:46:52 | 25.5435 | 0.81567 | 22.4397 | 128.4327 | 327.0990 | 1.19252 | 3.500 |
| 2025 Oct 17 17:56 | 2025 Oct 07 07:03:51 | 25.5644 | 0.81559 | 22.5448 | 125.6834 | 327.0990 | 1.19252 | 3.500 |
| 2025 Oct 16 17:56 | 2025 Oct 07 07:03:51 | 25.5644 | 0.81559 | 22.5448 | 125.6834 | 327.0990 | 1.19252 | 3.500 |
| 2025 Oct 15 17:56 | 2025 Oct 07 07:03:51 | 25.5644 | 0.81559 | 22.5448 | 125.6834 | 327.0990 | 1.19252 | 3.500 |
| 2025 Oct 14 17:56 | 2025 Oct 07 07:03:51 | 25.5644 | 0.81559 | 22.5448 | 125.6834 | 327.0990 | 1.19252 | 3.500 |
| 2025 Oct 12 17:56 | 2025 Oct 07 07:03:51 | 25.5644 | 0.81559 | 22.5448 | 125.6834 | 327.0990 | 1.19252 | 3.500 |
| 2025 Oct 11 17:57 | 2025 Oct 07 07:03:51 | 25.5644 | 0.81559 | 22.5448 | 125.6834 | 327.0990 | 1.19252 | 3.500 |
| 2025 Oct 09 17:56 | 2025 Oct 07 07:03:51 | 25.5644 | 0.81559 | 22.5448 | 125.6834 | 327.0990 | 1.19252 | 3.500 |