Orbital elements of DELTA 1 R/B
Launched | 18 August 1964 |
Flight ended | – |
Launch site | Air Force Eastern Test Range, Florida, USA |
Owner | United States |
NORAD ID | 862 |
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 11 18:21:49 | 16.8316 | 0.71114 | 2.8355 | 255.5296 | 22.2777 | 2.05106 | – |
2025 Oct 20 17:56 | 2025 Oct 11 18:21:49 | 16.8316 | 0.71114 | 2.8355 | 255.5296 | 22.2777 | 2.05106 | – |
2025 Oct 19 17:56 | 2025 Oct 11 18:21:49 | 16.8316 | 0.71114 | 2.8355 | 255.5296 | 22.2777 | 2.05106 | – |
2025 Oct 18 17:56 | 2025 Oct 11 18:21:49 | 16.8316 | 0.71114 | 2.8355 | 255.5296 | 22.2777 | 2.05106 | – |
2025 Oct 17 17:56 | 2025 Oct 07 09:05:37 | 16.8280 | 0.71116 | 2.9148 | 253.2720 | 22.2777 | 2.05106 | – |
2025 Oct 16 17:56 | 2025 Oct 07 09:05:37 | 16.8280 | 0.71116 | 2.9148 | 253.2720 | 22.2777 | 2.05106 | – |
2025 Oct 15 17:56 | 2025 Oct 07 09:05:37 | 16.8280 | 0.71116 | 2.9148 | 253.2720 | 22.2777 | 2.05106 | – |
2025 Oct 14 17:56 | 2025 Oct 07 09:05:37 | 16.8280 | 0.71116 | 2.9148 | 253.2720 | 22.2777 | 2.05106 | – |
2025 Oct 12 17:56 | 2025 Oct 07 09:05:37 | 16.8280 | 0.71116 | 2.9148 | 253.2720 | 22.2777 | 2.05106 | – |
2025 Oct 11 17:57 | 2025 Oct 07 09:05:37 | 16.8280 | 0.71116 | 2.9148 | 253.2720 | 22.2777 | 2.05106 | – |
2025 Oct 09 17:56 | 2025 Oct 07 09:05:37 | 16.8280 | 0.71116 | 2.9148 | 253.2720 | 22.2777 | 2.05106 | – |
2025 Oct 08 17:56 | 2025 Oct 07 09:05:37 | 16.8280 | 0.71116 | 2.9148 | 253.2720 | 22.2777 | 2.05106 | – |
2025 Oct 07 17:56 | 2025 Oct 07 09:05:37 | 16.8280 | 0.71116 | 2.9148 | 253.2720 | 22.2777 | 2.05106 | – |
2025 Oct 05 17:56 | 2025 Sep 23 17:35:26 | 16.8114 | 0.71127 | 3.1619 | 246.2405 | 22.2777 | 2.05106 | – |
2025 Oct 04 17:57 | 2025 Sep 23 17:35:26 | 16.8114 | 0.71127 | 3.1619 | 246.2405 | 22.2777 | 2.05106 | – |
2025 Oct 03 17:57 | 2025 Sep 23 17:35:26 | 16.8114 | 0.71127 | 3.1619 | 246.2405 | 22.2777 | 2.05106 | – |
2025 Oct 02 17:56 | 2025 Sep 23 17:35:26 | 16.8114 | 0.71127 | 3.1619 | 246.2405 | 22.2777 | 2.05106 | – |
2025 Sep 30 17:56 | 2025 Sep 23 17:35:26 | 16.8114 | 0.71127 | 3.1619 | 246.2405 | 22.2777 | 2.05106 | – |
2025 Sep 29 17:56 | 2025 Sep 23 17:35:26 | 16.8114 | 0.71127 | 3.1619 | 246.2405 | 22.2777 | 2.05106 | – |
2025 Sep 28 17:56 | 2025 Sep 23 17:35:26 | 16.8114 | 0.71127 | 3.1619 | 246.2405 | 22.2777 | 2.05106 | – |
2025 Sep 27 17:56 | 2025 Sep 23 17:35:26 | 16.8114 | 0.71127 | 3.1619 | 246.2405 | 22.2777 | 2.05106 | – |
2025 Sep 26 17:56 | 2025 Sep 23 17:35:26 | 16.8114 | 0.71127 | 3.1619 | 246.2405 | 22.2777 | 2.05106 | – |
2025 Sep 25 17:56 | 2025 Sep 19 08:19:46 | 16.8044 | 0.71131 | 3.2413 | 243.9806 | 22.2777 | 2.05106 | – |
2025 Sep 24 17:56 | 2025 Sep 19 08:19:46 | 16.8044 | 0.71131 | 3.2413 | 243.9806 | 22.2777 | 2.05106 | – |