Orbital elements of DELTA 2 R/B(1)
| Launched | 8 September 1992 |
| Flight ended | – |
| Launch site | Air Force Eastern Test Range, Florida, USA |
| Owner | United States |
| NORAD ID | 22109 |
| 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 Dec 15 18:58 | 2025 Dec 11 16:22:54 | 19.7813 | 0.00321 | 6.5085 | 103.0059 | 257.3944 | 14.79719 | 4.743 |
| 2025 Dec 14 18:56 | 2025 Dec 11 16:22:54 | 19.7813 | 0.00321 | 6.5085 | 103.0059 | 257.3944 | 14.79719 | 4.743 |
| 2025 Dec 13 18:56 | 2025 Dec 11 16:22:54 | 19.7813 | 0.00321 | 6.5085 | 103.0059 | 257.3944 | 14.79719 | 4.743 |
| 2025 Dec 12 18:57 | 2025 Dec 11 16:22:54 | 19.7813 | 0.00321 | 6.5085 | 103.0059 | 257.3944 | 14.79719 | 4.743 |
| 2025 Dec 11 18:56 | 2025 Dec 07 02:20:38 | 19.7806 | 0.00321 | 8.5769 | 46.9146 | 257.3944 | 14.79719 | 4.743 |
| 2025 Dec 10 18:56 | 2025 Dec 07 02:20:38 | 19.7806 | 0.00321 | 8.5769 | 46.9146 | 257.3944 | 14.79719 | 4.743 |
| 2025 Dec 09 18:56 | 2025 Dec 07 02:20:38 | 19.7806 | 0.00321 | 8.5769 | 46.9146 | 257.3944 | 14.79719 | 4.743 |
| 2025 Dec 08 18:56 | 2025 Dec 07 02:20:38 | 19.7806 | 0.00321 | 8.5769 | 46.9146 | 257.3944 | 14.79719 | 4.743 |
| 2025 Dec 07 18:56 | 2025 Dec 07 02:20:38 | 19.7806 | 0.00321 | 8.5769 | 46.9146 | 257.3944 | 14.79719 | 4.743 |
| 2025 Dec 06 18:56 | 2025 Dec 01 21:44:20 | 19.7795 | 0.00319 | 10.9191 | 343.0232 | 257.3944 | 14.79719 | 4.743 |
| 2025 Dec 05 18:57 | 2025 Dec 01 21:44:20 | 19.7795 | 0.00319 | 10.9191 | 343.0232 | 257.3944 | 14.79719 | 4.743 |
| 2025 Dec 04 18:57 | 2025 Dec 01 21:44:20 | 19.7795 | 0.00319 | 10.9191 | 343.0232 | 257.3944 | 14.79719 | 4.743 |
| 2025 Dec 03 18:56 | 2025 Dec 01 21:44:20 | 19.7795 | 0.00319 | 10.9191 | 343.0232 | 257.3944 | 14.79719 | 4.743 |
| 2025 Dec 02 18:56 | 2025 Dec 01 21:44:20 | 19.7795 | 0.00319 | 10.9191 | 343.0232 | 257.3944 | 14.79719 | 4.743 |
| 2025 Nov 30 18:57 | 2025 Nov 25 00:40:35 | 19.7808 | 0.00318 | 14.0216 | 257.9493 | 257.3944 | 14.79719 | 4.743 |
| 2025 Nov 29 18:56 | 2025 Nov 25 00:40:35 | 19.7808 | 0.00318 | 14.0216 | 257.9493 | 257.3944 | 14.79719 | 4.743 |
| 2025 Nov 28 18:57 | 2025 Nov 25 00:40:35 | 19.7808 | 0.00318 | 14.0216 | 257.9493 | 257.3944 | 14.79719 | 4.743 |
| 2025 Nov 27 18:57 | 2025 Nov 25 00:40:35 | 19.7808 | 0.00318 | 14.0216 | 257.9493 | 257.3944 | 14.79719 | 4.743 |
| 2025 Nov 26 18:57 | 2025 Nov 25 00:40:35 | 19.7808 | 0.00318 | 14.0216 | 257.9493 | 257.3944 | 14.79719 | 4.743 |
| 2025 Nov 25 18:57 | 2025 Nov 25 00:40:35 | 19.7808 | 0.00318 | 14.0216 | 257.9493 | 257.3944 | 14.79719 | 4.743 |
| 2025 Nov 24 18:56 | 2025 Nov 20 02:32:37 | 19.7818 | 0.00319 | 16.2419 | 196.9564 | 257.3944 | 14.79719 | 4.743 |
| 2025 Nov 23 18:57 | 2025 Nov 20 02:32:37 | 19.7818 | 0.00319 | 16.2419 | 196.9564 | 257.3944 | 14.79719 | 4.743 |
| 2025 Nov 21 18:57 | 2025 Nov 20 02:32:37 | 19.7818 | 0.00319 | 16.2419 | 196.9564 | 257.3944 | 14.79719 | 4.743 |
| 2025 Nov 20 18:56 | 2025 Nov 20 02:32:37 | 19.7818 | 0.00319 | 16.2419 | 196.9564 | 257.3944 | 14.79719 | 4.743 |
| 2025 Nov 18 18:57 | 2025 Nov 08 17:03:07 | 19.7831 | 0.00321 | 21.3816 | 57.2349 | 257.3944 | 14.79719 | 4.743 |