Orbital elements of DELTA 1 R/B(2)
| Launched | 2 August 1981 |
| Flight ended | – |
| Launch site | Air Force Western Test Range, California, USA |
| Owner | United States |
| NORAD ID | 12679 |
| 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 22 17:56 | 2025 Oct 17 07:10:48 | 90.9159 | 0.61898 | 3.0924 | 294.8861 | 14.4113 | 3.53032 | 7.743 |
| 2025 Oct 21 17:56 | 2025 Oct 17 07:10:48 | 90.9159 | 0.61898 | 3.0924 | 294.8861 | 14.4113 | 3.53032 | 7.743 |
| 2025 Oct 20 17:56 | 2025 Oct 17 07:10:48 | 90.9159 | 0.61898 | 3.0924 | 294.8861 | 14.4113 | 3.53032 | 7.743 |
| 2025 Oct 19 17:56 | 2025 Oct 17 07:10:48 | 90.9159 | 0.61898 | 3.0924 | 294.8861 | 14.4113 | 3.53032 | 7.743 |
| 2025 Oct 18 17:56 | 2025 Oct 17 07:10:48 | 90.9159 | 0.61898 | 3.0924 | 294.8861 | 14.4113 | 3.53032 | 7.743 |
| 2025 Oct 17 17:56 | 2025 Oct 06 06:01:42 | 90.9078 | 0.61901 | 3.0856 | 298.5959 | 14.4113 | 3.53032 | 7.743 |
| 2025 Oct 16 17:56 | 2025 Oct 06 06:01:42 | 90.9078 | 0.61901 | 3.0856 | 298.5959 | 14.4113 | 3.53032 | 7.743 |
| 2025 Oct 15 17:56 | 2025 Oct 06 06:01:42 | 90.9078 | 0.61901 | 3.0856 | 298.5959 | 14.4113 | 3.53032 | 7.743 |
| 2025 Oct 14 17:56 | 2025 Oct 06 06:01:42 | 90.9078 | 0.61901 | 3.0856 | 298.5959 | 14.4113 | 3.53032 | 7.743 |
| 2025 Oct 12 17:56 | 2025 Oct 06 06:01:42 | 90.9078 | 0.61901 | 3.0856 | 298.5959 | 14.4113 | 3.53032 | 7.743 |
| 2025 Oct 11 17:57 | 2025 Oct 06 06:01:42 | 90.9078 | 0.61901 | 3.0856 | 298.5959 | 14.4113 | 3.53032 | 7.743 |
| 2025 Oct 09 17:56 | 2025 Oct 06 06:01:42 | 90.9078 | 0.61901 | 3.0856 | 298.5959 | 14.4113 | 3.53032 | 7.743 |
| 2025 Oct 08 17:56 | 2025 Oct 06 06:01:42 | 90.9078 | 0.61901 | 3.0856 | 298.5959 | 14.4113 | 3.53032 | 7.743 |
| 2025 Oct 07 17:56 | 2025 Oct 06 06:01:42 | 90.9078 | 0.61901 | 3.0856 | 298.5959 | 14.4113 | 3.53032 | 7.743 |
| 2025 Oct 05 17:56 | 2025 Sep 22 15:41:06 | 90.8926 | 0.61912 | 3.0771 | 303.1581 | 14.4113 | 3.53032 | 7.743 |
| 2025 Oct 04 17:57 | 2025 Sep 22 15:41:06 | 90.8926 | 0.61912 | 3.0771 | 303.1581 | 14.4113 | 3.53032 | 7.743 |
| 2025 Oct 03 17:57 | 2025 Sep 22 15:41:06 | 90.8926 | 0.61912 | 3.0771 | 303.1581 | 14.4113 | 3.53032 | 7.743 |
| 2025 Oct 02 17:56 | 2025 Sep 22 15:41:06 | 90.8926 | 0.61912 | 3.0771 | 303.1581 | 14.4113 | 3.53032 | 7.743 |
| 2025 Sep 30 17:56 | 2025 Sep 22 15:41:06 | 90.8926 | 0.61912 | 3.0771 | 303.1581 | 14.4113 | 3.53032 | 7.743 |
| 2025 Sep 29 17:56 | 2025 Sep 22 15:41:06 | 90.8926 | 0.61912 | 3.0771 | 303.1581 | 14.4113 | 3.53032 | 7.743 |
| 2025 Sep 28 17:56 | 2025 Sep 22 15:41:06 | 90.8926 | 0.61912 | 3.0771 | 303.1581 | 14.4113 | 3.53032 | 7.743 |
| 2025 Sep 27 17:56 | 2025 Sep 22 15:41:06 | 90.8926 | 0.61912 | 3.0771 | 303.1581 | 14.4113 | 3.53032 | 7.743 |
| 2025 Sep 26 17:56 | 2025 Sep 22 15:41:06 | 90.8926 | 0.61912 | 3.0771 | 303.1581 | 14.4113 | 3.53032 | 7.743 |
| 2025 Sep 25 17:56 | 2025 Sep 18 09:42:11 | 90.8939 | 0.61915 | 3.0745 | 304.5916 | 14.4113 | 3.53032 | 7.743 |