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 Oct 21 17:56 | 2025 Oct 18 07:30:53 | 26.3871 | 0.05131 | 20.7026 | 207.8508 | 261.0803 | 12.94601 | 4.743 |
| 2025 Oct 20 17:56 | 2025 Oct 18 07:30:53 | 26.3871 | 0.05131 | 20.7026 | 207.8508 | 261.0803 | 12.94601 | 4.743 |
| 2025 Oct 19 17:56 | 2025 Oct 18 07:30:53 | 26.3871 | 0.05131 | 20.7026 | 207.8508 | 261.0803 | 12.94601 | 4.743 |
| 2025 Oct 18 17:56 | 2025 Oct 18 07:30:53 | 26.3871 | 0.05131 | 20.7026 | 207.8508 | 261.0803 | 12.94601 | 4.743 |
| 2025 Oct 17 17:56 | 2025 Oct 07 06:31:15 | 26.3852 | 0.05133 | 0.1879 | 119.9726 | 261.0803 | 12.94601 | 4.743 |
| 2025 Oct 16 17:56 | 2025 Oct 07 06:31:15 | 26.3852 | 0.05133 | 0.1879 | 119.9726 | 261.0803 | 12.94601 | 4.743 |
| 2025 Oct 15 17:56 | 2025 Oct 07 06:31:15 | 26.3852 | 0.05133 | 0.1879 | 119.9726 | 261.0803 | 12.94601 | 4.743 |
| 2025 Oct 14 17:56 | 2025 Oct 07 06:31:15 | 26.3852 | 0.05133 | 0.1879 | 119.9726 | 261.0803 | 12.94601 | 4.743 |
| 2025 Oct 12 17:56 | 2025 Oct 07 06:31:15 | 26.3852 | 0.05133 | 0.1879 | 119.9726 | 261.0803 | 12.94601 | 4.743 |
| 2025 Oct 11 17:57 | 2025 Oct 07 06:31:15 | 26.3852 | 0.05133 | 0.1879 | 119.9726 | 261.0803 | 12.94601 | 4.743 |
| 2025 Oct 09 17:56 | 2025 Oct 07 06:31:15 | 26.3852 | 0.05133 | 0.1879 | 119.9726 | 261.0803 | 12.94601 | 4.743 |
| 2025 Oct 08 17:56 | 2025 Oct 07 06:31:15 | 26.3852 | 0.05133 | 0.1879 | 119.9726 | 261.0803 | 12.94601 | 4.743 |
| 2025 Oct 07 17:56 | 2025 Oct 07 06:31:15 | 26.3852 | 0.05133 | 0.1879 | 119.9726 | 261.0803 | 12.94601 | 4.743 |
| 2025 Oct 05 17:56 | 2025 Sep 25 21:15:31 | 26.3850 | 0.05134 | 3.7821 | 29.3722 | 261.0803 | 12.94601 | 4.743 |
| 2025 Oct 04 17:57 | 2025 Sep 25 21:15:31 | 26.3850 | 0.05134 | 3.7821 | 29.3722 | 261.0803 | 12.94601 | 4.743 |
| 2025 Oct 03 17:57 | 2025 Sep 25 21:15:31 | 26.3850 | 0.05134 | 3.7821 | 29.3722 | 261.0803 | 12.94601 | 4.743 |
| 2025 Oct 02 17:56 | 2025 Sep 25 21:15:31 | 26.3850 | 0.05134 | 3.7821 | 29.3722 | 261.0803 | 12.94601 | 4.743 |
| 2025 Sep 30 17:56 | 2025 Sep 25 21:15:31 | 26.3850 | 0.05134 | 3.7821 | 29.3722 | 261.0803 | 12.94601 | 4.743 |
| 2025 Sep 29 17:56 | 2025 Sep 25 21:15:31 | 26.3850 | 0.05134 | 3.7821 | 29.3722 | 261.0803 | 12.94601 | 4.743 |
| 2025 Sep 28 17:56 | 2025 Sep 25 21:15:31 | 26.3850 | 0.05134 | 3.7821 | 29.3722 | 261.0803 | 12.94601 | 4.743 |
| 2025 Sep 27 17:56 | 2025 Sep 25 21:15:31 | 26.3850 | 0.05134 | 3.7821 | 29.3722 | 261.0803 | 12.94601 | 4.743 |
| 2025 Sep 26 17:56 | 2025 Sep 25 21:15:31 | 26.3850 | 0.05134 | 3.7821 | 29.3722 | 261.0803 | 12.94601 | 4.743 |
| 2025 Sep 25 17:56 | 2025 Sep 20 00:43:12 | 26.3857 | 0.05134 | 5.6305 | 342.7661 | 261.0803 | 12.94601 | 4.743 |
| 2025 Sep 24 17:56 | 2025 Sep 20 00:43:12 | 26.3857 | 0.05134 | 5.6305 | 342.7661 | 261.0803 | 12.94601 | 4.743 |