Orbital elements of DELTA 2 R/B(1)
| Launched | 28 January 2003 |
| Flight ended | – |
| Launch site | Air Force Eastern Test Range, Florida, USA |
| Owner | United States |
| NORAD ID | 27665 |
| 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 Apr 10 17:56 | 2025 Apr 05 21:54:55 | 39.5771 | 0.00070 | 23.6716 | 80.0705 | 18.5441 | 14.29361 | 4.743 |
| 2025 Apr 09 17:57 | 2025 Apr 05 21:54:55 | 39.5771 | 0.00070 | 23.6716 | 80.0705 | 18.5441 | 14.29361 | 4.743 |
| 2025 Apr 08 17:57 | 2025 Apr 05 21:54:55 | 39.5771 | 0.00070 | 23.6716 | 80.0705 | 18.5441 | 14.29361 | 4.743 |
| 2025 Apr 07 17:56 | 2025 Apr 05 21:54:55 | 39.5771 | 0.00070 | 23.6716 | 80.0705 | 18.5441 | 14.29361 | 4.743 |
| 2025 Apr 06 17:56 | 2025 Apr 05 21:54:55 | 39.5771 | 0.00070 | 23.6716 | 80.0705 | 18.5441 | 14.29361 | 4.743 |
| 2025 Apr 05 17:56 | 2025 Apr 01 12:37:24 | 39.5771 | 0.00072 | 1.1630 | 47.6672 | 18.5441 | 14.29361 | 4.743 |
| 2025 Apr 04 17:56 | 2025 Apr 01 12:37:24 | 39.5771 | 0.00072 | 1.1630 | 47.6672 | 18.5441 | 14.29361 | 4.743 |
| 2025 Apr 03 17:56 | 2025 Apr 01 12:37:24 | 39.5771 | 0.00072 | 1.1630 | 47.6672 | 18.5441 | 14.29361 | 4.743 |
| 2025 Apr 02 17:57 | 2025 Apr 01 12:37:24 | 39.5771 | 0.00072 | 1.1630 | 47.6672 | 18.5441 | 14.29361 | 4.743 |
| 2025 Apr 01 17:56 | 2025 Apr 01 12:37:24 | 39.5771 | 0.00072 | 1.1630 | 47.6672 | 18.5441 | 14.29361 | 4.743 |
| 2025 Mar 31 17:56 | 2025 Mar 26 03:44:18 | 39.5762 | 0.00079 | 3.3286 | 3.4445 | 18.5441 | 14.29361 | 4.743 |
| 2025 Mar 30 17:57 | 2025 Mar 26 03:44:18 | 39.5762 | 0.00079 | 3.3286 | 3.4445 | 18.5441 | 14.29361 | 4.743 |
| 2025 Mar 29 18:56 | 2025 Mar 26 03:44:18 | 39.5762 | 0.00079 | 3.3286 | 3.4445 | 18.5441 | 14.29361 | 4.743 |
| 2025 Mar 28 18:57 | 2025 Mar 26 03:44:18 | 39.5762 | 0.00079 | 3.3286 | 3.4445 | 18.5441 | 14.29361 | 4.743 |
| 2025 Mar 27 18:56 | 2025 Mar 26 03:44:18 | 39.5762 | 0.00079 | 3.3286 | 3.4445 | 18.5441 | 14.29361 | 4.743 |
| 2025 Mar 26 18:57 | 2025 Mar 26 03:44:18 | 39.5762 | 0.00079 | 3.3286 | 3.4445 | 18.5441 | 14.29361 | 4.743 |
| 2025 Mar 25 18:57 | 2025 Mar 21 09:53:22 | 39.5753 | 0.00084 | 4.9412 | 333.3421 | 18.5441 | 14.29361 | 4.743 |
| 2025 Mar 24 18:57 | 2025 Mar 21 09:53:22 | 39.5753 | 0.00084 | 4.9412 | 333.3421 | 18.5441 | 14.29361 | 4.743 |
| 2025 Mar 23 18:58 | 2025 Mar 21 09:53:22 | 39.5753 | 0.00084 | 4.9412 | 333.3421 | 18.5441 | 14.29361 | 4.743 |
| 2025 Mar 22 18:58 | 2025 Mar 21 09:53:22 | 39.5753 | 0.00084 | 4.9412 | 333.3421 | 18.5441 | 14.29361 | 4.743 |
| 2025 Mar 21 18:57 | 2025 Mar 21 09:53:22 | 39.5753 | 0.00084 | 4.9412 | 333.3421 | 18.5441 | 14.29361 | 4.743 |
| 2025 Mar 20 18:57 | 2025 Mar 16 10:51:08 | 39.5748 | 0.00088 | 6.6274 | 303.5250 | 18.5441 | 14.29361 | 4.743 |
| 2025 Mar 19 18:57 | 2025 Mar 16 10:51:08 | 39.5748 | 0.00088 | 6.6274 | 303.5250 | 18.5441 | 14.29361 | 4.743 |
| 2025 Mar 18 18:56 | 2025 Mar 16 10:51:08 | 39.5748 | 0.00088 | 6.6274 | 303.5250 | 18.5441 | 14.29361 | 4.743 |
| 2025 Mar 17 18:56 | 2025 Mar 16 10:51:08 | 39.5748 | 0.00088 | 6.6274 | 303.5250 | 18.5441 | 14.29361 | 4.743 |
| 2025 Mar 16 18:56 | 2025 Mar 16 10:51:08 | 39.5748 | 0.00088 | 6.6274 | 303.5250 | 18.5441 | 14.29361 | 4.743 |
| 2025 Mar 15 18:56 | 2025 Mar 10 12:15:02 | 39.5747 | 0.00090 | 8.6473 | 268.7272 | 18.5441 | 14.29361 | 4.743 |
| 2025 Mar 14 18:56 | 2025 Mar 10 12:15:02 | 39.5747 | 0.00090 | 8.6473 | 268.7272 | 18.5441 | 14.29361 | 4.743 |