Orbital elements of DELTA 2 R/B(1)
| Launched | 9 June 1998 |
| Flight ended | – |
| Launch site | Air Force Eastern Test Range, Florida, USA |
| Owner | United States |
| NORAD ID | 25359 |
| 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 May 09 17:57 | 2025 May 09 01:54:28 | 26.3872 | 0.05132 | 23.9127 | 356.6654 | 162.9204 | 12.94591 | 4.743 |
| 2025 May 08 17:56 | 2025 May 03 10:50:10 | 26.3890 | 0.05133 | 1.6890 | 311.8668 | 162.9204 | 12.94591 | 4.743 |
| 2025 May 07 17:56 | 2025 May 03 10:50:10 | 26.3890 | 0.05133 | 1.6890 | 311.8668 | 162.9204 | 12.94591 | 4.743 |
| 2025 May 06 17:57 | 2025 May 03 10:50:10 | 26.3890 | 0.05133 | 1.6890 | 311.8668 | 162.9204 | 12.94591 | 4.743 |
| 2025 May 05 17:56 | 2025 May 03 10:50:10 | 26.3890 | 0.05133 | 1.6890 | 311.8668 | 162.9204 | 12.94591 | 4.743 |
| 2025 May 04 17:57 | 2025 May 03 10:50:10 | 26.3890 | 0.05133 | 1.6890 | 311.8668 | 162.9204 | 12.94591 | 4.743 |
| 2025 May 03 17:57 | 2025 May 03 10:50:10 | 26.3890 | 0.05133 | 1.6890 | 311.8668 | 162.9204 | 12.94591 | 4.743 |
| 2025 May 01 17:56 | 2025 Apr 22 00:22:35 | 26.3861 | 0.05133 | 5.2982 | 220.8580 | 162.9204 | 12.94591 | 4.743 |
| 2025 Apr 30 17:56 | 2025 Apr 22 00:22:35 | 26.3861 | 0.05133 | 5.2982 | 220.8580 | 162.9204 | 12.94591 | 4.743 |
| 2025 Apr 29 17:57 | 2025 Apr 22 00:22:35 | 26.3861 | 0.05133 | 5.2982 | 220.8580 | 162.9204 | 12.94591 | 4.743 |
| 2025 Apr 27 17:56 | 2025 Apr 22 00:22:35 | 26.3861 | 0.05133 | 5.2982 | 220.8580 | 162.9204 | 12.94591 | 4.743 |
| 2025 Apr 26 17:57 | 2025 Apr 22 00:22:35 | 26.3861 | 0.05133 | 5.2982 | 220.8580 | 162.9204 | 12.94591 | 4.743 |
| 2025 Apr 25 17:56 | 2025 Apr 22 00:22:35 | 26.3861 | 0.05133 | 5.2982 | 220.8580 | 162.9204 | 12.94591 | 4.743 |
| 2025 Apr 24 17:56 | 2025 Apr 22 00:22:35 | 26.3861 | 0.05133 | 5.2982 | 220.8580 | 162.9204 | 12.94591 | 4.743 |
| 2025 Apr 23 17:57 | 2025 Apr 22 00:22:35 | 26.3861 | 0.05133 | 5.2982 | 220.8580 | 162.9204 | 12.94591 | 4.743 |
| 2025 Apr 22 17:56 | 2025 Apr 22 00:22:35 | 26.3861 | 0.05133 | 5.2982 | 220.8580 | 162.9204 | 12.94591 | 4.743 |
| 2025 Apr 21 17:57 | 2025 Apr 15 07:13:19 | 26.3830 | 0.05134 | 7.4178 | 167.4124 | 162.9204 | 12.94591 | 4.743 |
| 2025 Apr 20 17:56 | 2025 Apr 15 07:13:19 | 26.3830 | 0.05134 | 7.4178 | 167.4124 | 162.9204 | 12.94591 | 4.743 |
| 2025 Apr 19 17:56 | 2025 Apr 15 07:13:19 | 26.3830 | 0.05134 | 7.4178 | 167.4124 | 162.9204 | 12.94591 | 4.743 |
| 2025 Apr 18 17:57 | 2025 Apr 15 07:13:19 | 26.3830 | 0.05134 | 7.4178 | 167.4124 | 162.9204 | 12.94591 | 4.743 |
| 2025 Apr 17 17:56 | 2025 Apr 15 07:13:19 | 26.3830 | 0.05134 | 7.4178 | 167.4124 | 162.9204 | 12.94591 | 4.743 |
| 2025 Apr 16 17:57 | 2025 Apr 15 07:13:19 | 26.3830 | 0.05134 | 7.4178 | 167.4124 | 162.9204 | 12.94591 | 4.743 |
| 2025 Apr 15 17:56 | 2025 Apr 11 05:21:24 | 26.3817 | 0.05135 | 8.7051 | 134.9612 | 162.9204 | 12.94591 | 4.743 |
| 2025 Apr 14 17:56 | 2025 Apr 11 05:21:24 | 26.3817 | 0.05135 | 8.7051 | 134.9612 | 162.9204 | 12.94591 | 4.743 |