Orbital elements of DELTA 1 R/B(2)
| Launched | 15 August 1984 |
| Flight ended | – |
| Launch site | Air Force Eastern Test Range, Florida, USA |
| Owner | United States |
| NORAD ID | 15206 |
| 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 27 18:57 | 2025 Oct 21 15:41:42 | 26.8284 | 0.77226 | 11.2463 | 203.5607 | 81.2982 | 1.58860 | 5.743 |
| 2025 Oct 26 18:57 | 2025 Oct 21 15:41:42 | 26.8284 | 0.77226 | 11.2463 | 203.5607 | 81.2982 | 1.58860 | 5.743 |
| 2025 Oct 25 17:57 | 2025 Oct 21 15:41:42 | 26.8284 | 0.77226 | 11.2463 | 203.5607 | 81.2982 | 1.58860 | 5.743 |
| 2025 Oct 24 17:57 | 2025 Oct 21 15:41:42 | 26.8284 | 0.77226 | 11.2463 | 203.5607 | 81.2982 | 1.58860 | 5.743 |
| 2025 Oct 22 17:56 | 2025 Oct 11 14:28:16 | 26.8561 | 0.77193 | 11.3949 | 199.8516 | 81.2982 | 1.58860 | 5.743 |
| 2025 Oct 21 17:56 | 2025 Oct 11 14:28:16 | 26.8561 | 0.77193 | 11.3949 | 199.8516 | 81.2982 | 1.58860 | 5.743 |
| 2025 Oct 20 17:56 | 2025 Oct 11 14:28:16 | 26.8561 | 0.77193 | 11.3949 | 199.8516 | 81.2982 | 1.58860 | 5.743 |
| 2025 Oct 19 17:56 | 2025 Oct 11 14:28:16 | 26.8561 | 0.77193 | 11.3949 | 199.8516 | 81.2982 | 1.58860 | 5.743 |
| 2025 Oct 18 17:56 | 2025 Oct 11 14:28:16 | 26.8561 | 0.77193 | 11.3949 | 199.8516 | 81.2982 | 1.58860 | 5.743 |
| 2025 Oct 17 17:56 | 2025 Oct 05 22:48:59 | 26.8581 | 0.77181 | 11.4787 | 197.7465 | 81.2982 | 1.58860 | 5.743 |
| 2025 Oct 16 17:56 | 2025 Oct 05 22:48:59 | 26.8581 | 0.77181 | 11.4787 | 197.7465 | 81.2982 | 1.58860 | 5.743 |
| 2025 Oct 15 17:56 | 2025 Oct 05 22:48:59 | 26.8581 | 0.77181 | 11.4787 | 197.7465 | 81.2982 | 1.58860 | 5.743 |
| 2025 Oct 14 17:56 | 2025 Oct 05 22:48:59 | 26.8581 | 0.77181 | 11.4787 | 197.7465 | 81.2982 | 1.58860 | 5.743 |
| 2025 Oct 12 17:56 | 2025 Oct 05 22:48:59 | 26.8581 | 0.77181 | 11.4787 | 197.7465 | 81.2982 | 1.58860 | 5.743 |
| 2025 Oct 11 17:57 | 2025 Oct 05 22:48:59 | 26.8581 | 0.77181 | 11.4787 | 197.7465 | 81.2982 | 1.58860 | 5.743 |
| 2025 Oct 09 17:56 | 2025 Oct 05 22:48:59 | 26.8581 | 0.77181 | 11.4787 | 197.7465 | 81.2982 | 1.58860 | 5.743 |
| 2025 Oct 08 17:56 | 2025 Oct 05 22:48:59 | 26.8581 | 0.77181 | 11.4787 | 197.7465 | 81.2982 | 1.58860 | 5.743 |
| 2025 Oct 07 17:56 | 2025 Oct 05 22:48:59 | 26.8581 | 0.77181 | 11.4787 | 197.7465 | 81.2982 | 1.58860 | 5.743 |
| 2025 Oct 05 17:56 | 2025 Sep 24 00:29:09 | 26.8663 | 0.77157 | 11.6558 | 193.3612 | 81.2982 | 1.58860 | 5.743 |
| 2025 Oct 04 17:57 | 2025 Sep 24 00:29:09 | 26.8663 | 0.77157 | 11.6558 | 193.3612 | 81.2982 | 1.58860 | 5.743 |
| 2025 Oct 03 17:57 | 2025 Sep 24 00:29:09 | 26.8663 | 0.77157 | 11.6558 | 193.3612 | 81.2982 | 1.58860 | 5.743 |
| 2025 Oct 02 17:56 | 2025 Sep 24 00:29:09 | 26.8663 | 0.77157 | 11.6558 | 193.3612 | 81.2982 | 1.58860 | 5.743 |
| 2025 Sep 30 17:56 | 2025 Sep 24 00:29:09 | 26.8663 | 0.77157 | 11.6558 | 193.3612 | 81.2982 | 1.58860 | 5.743 |