Orbital elements of DELTA 1 R/B(2)
Launched | 13 November 1984 |
Flight ended | – |
Launch site | Air Force Eastern Test Range, Florida, USA |
Owner | United States |
NORAD ID | 15402 |
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 20 17:56 | 2025 Oct 18 05:38:59 | 23.4644 | 0.71354 | 0.1361 | 309.6525 | 6.7740 | 2.37986 | 7.243 |
2025 Oct 19 17:56 | 2025 Oct 18 05:38:59 | 23.4644 | 0.71354 | 0.1361 | 309.6525 | 6.7740 | 2.37986 | 7.243 |
2025 Oct 18 17:56 | 2025 Oct 18 05:38:59 | 23.4644 | 0.71354 | 0.1361 | 309.6525 | 6.7740 | 2.37986 | 7.243 |
2025 Oct 17 17:56 | 2025 Oct 07 07:28:39 | 23.4614 | 0.71358 | 0.4134 | 302.3513 | 6.7740 | 2.37986 | 7.243 |
2025 Oct 16 17:56 | 2025 Oct 07 07:28:39 | 23.4614 | 0.71358 | 0.4134 | 302.3513 | 6.7740 | 2.37986 | 7.243 |
2025 Oct 15 17:56 | 2025 Oct 07 07:28:39 | 23.4614 | 0.71358 | 0.4134 | 302.3513 | 6.7740 | 2.37986 | 7.243 |
2025 Oct 14 17:56 | 2025 Oct 07 07:28:39 | 23.4614 | 0.71358 | 0.4134 | 302.3513 | 6.7740 | 2.37986 | 7.243 |
2025 Oct 12 17:56 | 2025 Oct 07 07:28:39 | 23.4614 | 0.71358 | 0.4134 | 302.3513 | 6.7740 | 2.37986 | 7.243 |
2025 Oct 11 17:57 | 2025 Oct 07 07:28:39 | 23.4614 | 0.71358 | 0.4134 | 302.3513 | 6.7740 | 2.37986 | 7.243 |
2025 Oct 09 17:56 | 2025 Oct 07 07:28:39 | 23.4614 | 0.71358 | 0.4134 | 302.3513 | 6.7740 | 2.37986 | 7.243 |
2025 Oct 08 17:56 | 2025 Oct 07 07:28:39 | 23.4614 | 0.71358 | 0.4134 | 302.3513 | 6.7740 | 2.37986 | 7.243 |
2025 Oct 07 17:56 | 2025 Oct 07 07:28:39 | 23.4614 | 0.71358 | 0.4134 | 302.3513 | 6.7740 | 2.37986 | 7.243 |
2025 Oct 05 17:56 | 2025 Sep 24 06:52:34 | 23.4574 | 0.71367 | 0.7447 | 293.6518 | 6.7740 | 2.37986 | 7.243 |
2025 Oct 04 17:57 | 2025 Sep 24 06:52:34 | 23.4574 | 0.71367 | 0.7447 | 293.6518 | 6.7740 | 2.37986 | 7.243 |
2025 Oct 03 17:57 | 2025 Sep 24 06:52:34 | 23.4574 | 0.71367 | 0.7447 | 293.6518 | 6.7740 | 2.37986 | 7.243 |
2025 Oct 02 17:56 | 2025 Sep 24 06:52:34 | 23.4574 | 0.71367 | 0.7447 | 293.6518 | 6.7740 | 2.37986 | 7.243 |
2025 Sep 30 17:56 | 2025 Sep 24 06:52:34 | 23.4574 | 0.71367 | 0.7447 | 293.6518 | 6.7740 | 2.37986 | 7.243 |
2025 Sep 29 17:56 | 2025 Sep 24 06:52:34 | 23.4574 | 0.71367 | 0.7447 | 293.6518 | 6.7740 | 2.37986 | 7.243 |
2025 Sep 28 17:56 | 2025 Sep 24 06:52:34 | 23.4574 | 0.71367 | 0.7447 | 293.6518 | 6.7740 | 2.37986 | 7.243 |
2025 Sep 27 17:56 | 2025 Sep 24 06:52:34 | 23.4574 | 0.71367 | 0.7447 | 293.6518 | 6.7740 | 2.37986 | 7.243 |
2025 Sep 26 17:56 | 2025 Sep 24 06:52:34 | 23.4574 | 0.71367 | 0.7447 | 293.6518 | 6.7740 | 2.37986 | 7.243 |
2025 Sep 25 17:56 | 2025 Sep 18 19:46:54 | 23.4579 | 0.71375 | 0.8841 | 289.9870 | 6.7740 | 2.37986 | 7.243 |
2025 Sep 24 17:56 | 2025 Sep 18 19:46:54 | 23.4579 | 0.71375 | 0.8841 | 289.9870 | 6.7740 | 2.37986 | 7.243 |