Orbital elements of DELTA 4 R/B
Launched | 28 June 2012 |
Flight ended | – |
Launch site | Air Force Eastern Test Range, Florida, USA |
Owner | United States |
NORAD ID | 38529 |
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 Aug 30 17:56 | 2025 Aug 27 13:40:29 | 6.2850 | 0.01932 | 4.1689 | 172.0967 | 188.4126 | 1.03152 | 3.243 |
2025 Aug 29 17:56 | 2025 Aug 27 13:40:29 | 6.2850 | 0.01932 | 4.1689 | 172.0967 | 188.4126 | 1.03152 | 3.243 |
2025 Aug 28 17:57 | 2025 Aug 27 13:40:29 | 6.2850 | 0.01932 | 4.1689 | 172.0967 | 188.4126 | 1.03152 | 3.243 |
2025 Aug 27 17:56 | 2025 Aug 19 19:32:43 | 6.2670 | 0.01929 | 4.1739 | 171.8714 | 188.4126 | 1.03152 | 3.243 |
2025 Aug 26 17:56 | 2025 Aug 19 19:32:43 | 6.2670 | 0.01929 | 4.1739 | 171.8714 | 188.4126 | 1.03152 | 3.243 |
2025 Aug 25 17:56 | 2025 Aug 19 19:32:43 | 6.2670 | 0.01929 | 4.1739 | 171.8714 | 188.4126 | 1.03152 | 3.243 |
2025 Aug 24 17:56 | 2025 Aug 19 19:32:43 | 6.2670 | 0.01929 | 4.1739 | 171.8714 | 188.4126 | 1.03152 | 3.243 |
2025 Aug 23 17:56 | 2025 Aug 19 19:32:43 | 6.2670 | 0.01929 | 4.1739 | 171.8714 | 188.4126 | 1.03152 | 3.243 |
2025 Aug 22 17:56 | 2025 Aug 17 21:00:41 | 6.2627 | 0.01928 | 4.1752 | 171.8206 | 188.4126 | 1.03152 | 3.243 |
2025 Aug 20 17:56 | 2025 Aug 17 21:00:41 | 6.2627 | 0.01928 | 4.1752 | 171.8206 | 188.4126 | 1.03152 | 3.243 |
2025 Aug 19 17:56 | 2025 Aug 17 21:00:41 | 6.2627 | 0.01928 | 4.1752 | 171.8206 | 188.4126 | 1.03152 | 3.243 |
2025 Aug 18 17:56 | 2025 Aug 17 21:00:41 | 6.2627 | 0.01928 | 4.1752 | 171.8206 | 188.4126 | 1.03152 | 3.243 |
2025 Aug 16 17:56 | 2025 Aug 11 02:09:21 | 6.2476 | 0.01926 | 4.1796 | 171.6585 | 188.4126 | 1.03152 | 3.243 |
2025 Aug 15 17:57 | 2025 Aug 11 02:09:21 | 6.2476 | 0.01926 | 4.1796 | 171.6585 | 188.4126 | 1.03152 | 3.243 |
2025 Aug 14 17:56 | 2025 Aug 11 02:09:21 | 6.2476 | 0.01926 | 4.1796 | 171.6585 | 188.4126 | 1.03152 | 3.243 |
2025 Aug 13 17:58 | 2025 Aug 11 02:09:21 | 6.2476 | 0.01926 | 4.1796 | 171.6585 | 188.4126 | 1.03152 | 3.243 |
2025 Aug 12 17:56 | 2025 Aug 11 02:09:21 | 6.2476 | 0.01926 | 4.1796 | 171.6585 | 188.4126 | 1.03152 | 3.243 |
2025 Aug 11 17:56 | 2025 Aug 06 05:49:19 | 6.2364 | 0.01926 | 4.1826 | 171.5366 | 188.4126 | 1.03152 | 3.243 |
2025 Aug 10 17:57 | 2025 Aug 06 05:49:19 | 6.2364 | 0.01926 | 4.1826 | 171.5366 | 188.4126 | 1.03152 | 3.243 |
2025 Aug 09 17:56 | 2025 Aug 06 05:49:19 | 6.2364 | 0.01926 | 4.1826 | 171.5366 | 188.4126 | 1.03152 | 3.243 |
2025 Aug 08 17:56 | 2025 Aug 06 05:49:19 | 6.2364 | 0.01926 | 4.1826 | 171.5366 | 188.4126 | 1.03152 | 3.243 |
2025 Aug 07 17:56 | 2025 Aug 06 05:49:19 | 6.2364 | 0.01926 | 4.1826 | 171.5366 | 188.4126 | 1.03152 | 3.243 |
2025 Aug 05 17:56 | 2025 Jul 31 10:13:30 | 6.2229 | 0.01924 | 4.1863 | 171.3769 | 188.4126 | 1.03152 | 3.243 |
2025 Aug 04 17:56 | 2025 Jul 31 10:13:30 | 6.2229 | 0.01924 | 4.1863 | 171.3769 | 188.4126 | 1.03152 | 3.243 |
2025 Aug 03 17:56 | 2025 Jul 31 10:13:30 | 6.2229 | 0.01924 | 4.1863 | 171.3769 | 188.4126 | 1.03152 | 3.243 |