Orbital elements of DELTA 2 R/B
| Launched | 24 July 1999 |
| Flight ended | – |
| Launch site | Air Force Eastern Test Range, Florida, USA |
| Owner | United States |
| NORAD ID | 25876 |
| 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 06 18:56 | 2025 Dec 06 04:46:30 | 51.7622 | 0.05048 | 20.9704 | 72.4901 | 293.0527 | 14.11376 | 4.743 |
| 2025 Dec 05 18:57 | 2025 Dec 05 04:58:54 | 51.7622 | 0.05048 | 21.2342 | 69.5665 | 293.0527 | 14.11376 | 4.743 |
| 2025 Dec 04 18:57 | 2025 Dec 04 03:29:19 | 51.7623 | 0.05048 | 21.5169 | 66.4368 | 293.0527 | 14.11376 | 4.743 |
| 2025 Dec 03 18:56 | 2025 Dec 03 10:29:36 | 51.7621 | 0.05048 | 21.7053 | 64.3516 | 293.0527 | 14.11376 | 4.743 |
| 2025 Dec 02 18:56 | 2025 Dec 02 10:41:58 | 51.7621 | 0.05048 | 21.9692 | 61.4303 | 293.0527 | 14.11376 | 4.743 |
| 2025 Nov 30 18:57 | 2025 Nov 30 09:24:44 | 51.7620 | 0.05049 | 22.5156 | 55.3791 | 293.0527 | 14.11376 | 4.743 |
| 2025 Nov 29 18:56 | 2025 Nov 29 04:31:10 | 51.7621 | 0.05049 | 22.8360 | 51.8322 | 293.0527 | 14.11376 | 4.743 |
| 2025 Nov 28 18:57 | 2025 Nov 28 04:43:31 | 51.7621 | 0.05049 | 23.0998 | 48.9108 | 293.0527 | 14.11376 | 4.743 |
| 2025 Nov 27 18:57 | 2025 Nov 27 06:37:50 | 51.7623 | 0.05049 | 23.3448 | 46.1993 | 293.0527 | 14.11376 | 4.743 |
| 2025 Nov 26 18:57 | 2025 Nov 26 11:56:06 | 51.7624 | 0.05049 | 23.5521 | 43.9032 | 293.0527 | 14.11376 | 4.743 |
| 2025 Nov 25 18:57 | 2025 Nov 25 08:44:29 | 51.7627 | 0.05049 | 23.8536 | 40.5653 | 293.0527 | 14.11376 | 4.743 |
| 2025 Nov 24 18:56 | 2025 Nov 24 02:08:54 | 51.7628 | 0.05049 | 0.1928 | 36.8093 | 293.0527 | 14.11376 | 4.743 |
| 2025 Nov 23 18:57 | 2025 Nov 23 07:27:09 | 51.7629 | 0.05049 | 0.4001 | 34.5140 | 293.0527 | 14.11376 | 4.743 |
| 2025 Nov 21 18:57 | 2025 Nov 21 02:45:51 | 51.7633 | 0.05049 | 0.9842 | 28.0432 | 293.0527 | 14.11376 | 4.743 |
| 2025 Nov 20 18:56 | 2025 Nov 19 21:52:14 | 51.7631 | 0.05049 | 1.3046 | 24.4908 | 293.0527 | 14.11376 | 4.743 |
| 2025 Nov 18 18:57 | 2025 Nov 18 11:52:39 | 51.7631 | 0.05049 | 1.6814 | 20.3173 | 293.0527 | 14.11376 | 4.743 |
| 2025 Nov 16 18:58 | 2025 Nov 15 14:11:31 | 51.7631 | 0.05049 | 2.4539 | 11.7694 | 293.0527 | 14.11376 | 4.743 |
| 2025 Nov 15 18:57 | 2025 Nov 14 16:05:46 | 51.7632 | 0.05049 | 2.6989 | 9.0593 | 293.0527 | 14.11376 | 4.743 |
| 2025 Nov 13 18:56 | 2025 Nov 13 12:54:05 | 51.7631 | 0.05049 | 3.0003 | 5.7206 | 293.0527 | 14.11376 | 4.743 |
| 2025 Nov 12 18:57 | 2025 Nov 12 06:18:26 | 51.7637 | 0.05048 | 3.3395 | 1.9591 | 293.0527 | 14.11376 | 4.743 |
| 2025 Nov 11 18:55 | 2025 Nov 11 06:30:43 | 51.7635 | 0.05048 | 3.6033 | 359.0377 | 293.0527 | 14.11376 | 4.743 |
| 2025 Nov 10 18:57 | 2025 Nov 08 17:19:22 | 51.7631 | 0.05048 | 4.2816 | 351.5247 | 293.0527 | 14.11376 | 4.743 |
| 2025 Nov 09 18:57 | 2025 Nov 08 17:19:22 | 51.7631 | 0.05048 | 4.2816 | 351.5247 | 293.0527 | 14.11376 | 4.743 |