Orbital elements of DELTA 4 R/B
Launched | 27 July 2014 |
Flight ended | – |
Launch site | Air Force Eastern Test Range, Florida, USA |
Owner | United States |
NORAD ID | 40102 |
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 Jun 30 17:56 | 2025 Jun 27 19:41:24 | 8.3615 | 0.00092 | 4.0550 | 300.9848 | 58.8504 | 0.98913 | 3.243 |
2025 Jun 29 17:56 | 2025 Jun 27 19:41:24 | 8.3615 | 0.00092 | 4.0550 | 300.9848 | 58.8504 | 0.98913 | 3.243 |
2025 Jun 28 17:56 | 2025 Jun 27 19:41:24 | 8.3615 | 0.00092 | 4.0550 | 300.9848 | 58.8504 | 0.98913 | 3.243 |
2025 Jun 27 17:56 | 2025 Jun 22 18:22:20 | 8.3502 | 0.00094 | 4.0582 | 301.1770 | 58.8504 | 0.98913 | 3.243 |
2025 Jun 26 17:56 | 2025 Jun 22 18:22:20 | 8.3502 | 0.00094 | 4.0582 | 301.1770 | 58.8504 | 0.98913 | 3.243 |
2025 Jun 25 17:56 | 2025 Jun 22 18:22:20 | 8.3502 | 0.00094 | 4.0582 | 301.1770 | 58.8504 | 0.98913 | 3.243 |
2025 Jun 24 17:56 | 2025 Jun 22 18:22:20 | 8.3502 | 0.00094 | 4.0582 | 301.1770 | 58.8504 | 0.98913 | 3.243 |
2025 Jun 23 17:56 | 2025 Jun 22 18:22:20 | 8.3502 | 0.00094 | 4.0582 | 301.1770 | 58.8504 | 0.98913 | 3.243 |
2025 Jun 22 17:56 | 2025 Jun 16 16:47:46 | 8.3366 | 0.00095 | 4.0620 | 300.6687 | 58.8504 | 0.98913 | 3.243 |
2025 Jun 21 17:56 | 2025 Jun 16 16:47:46 | 8.3366 | 0.00095 | 4.0620 | 300.6687 | 58.8504 | 0.98913 | 3.243 |
2025 Jun 20 17:57 | 2025 Jun 16 16:47:46 | 8.3366 | 0.00095 | 4.0620 | 300.6687 | 58.8504 | 0.98913 | 3.243 |
2025 Jun 19 17:56 | 2025 Jun 16 16:47:46 | 8.3366 | 0.00095 | 4.0620 | 300.6687 | 58.8504 | 0.98913 | 3.243 |
2025 Jun 18 17:56 | 2025 Jun 16 16:47:46 | 8.3366 | 0.00095 | 4.0620 | 300.6687 | 58.8504 | 0.98913 | 3.243 |
2025 Jun 17 17:56 | 2025 Jun 16 16:47:46 | 8.3366 | 0.00095 | 4.0620 | 300.6687 | 58.8504 | 0.98913 | 3.243 |
2025 Jun 16 17:56 | 2025 Jun 10 15:12:47 | 8.3224 | 0.00096 | 4.0658 | 300.0720 | 58.8504 | 0.98913 | 3.243 |
2025 Jun 15 17:56 | 2025 Jun 10 15:12:47 | 8.3224 | 0.00096 | 4.0658 | 300.0720 | 58.8504 | 0.98913 | 3.243 |
2025 Jun 14 17:56 | 2025 Jun 10 15:12:47 | 8.3224 | 0.00096 | 4.0658 | 300.0720 | 58.8504 | 0.98913 | 3.243 |
2025 Jun 13 17:56 | 2025 Jun 10 15:12:47 | 8.3224 | 0.00096 | 4.0658 | 300.0720 | 58.8504 | 0.98913 | 3.243 |
2025 Jun 12 17:56 | 2025 Jun 10 15:12:47 | 8.3224 | 0.00096 | 4.0658 | 300.0720 | 58.8504 | 0.98913 | 3.243 |
2025 Jun 11 17:56 | 2025 Jun 04 13:38:22 | 8.3081 | 0.00096 | 4.0695 | 300.2281 | 58.8504 | 0.98913 | 3.243 |
2025 Jun 10 17:56 | 2025 Jun 04 13:38:22 | 8.3081 | 0.00096 | 4.0695 | 300.2281 | 58.8504 | 0.98913 | 3.243 |
2025 Jun 09 17:56 | 2025 Jun 04 13:38:22 | 8.3081 | 0.00096 | 4.0695 | 300.2281 | 58.8504 | 0.98913 | 3.243 |
2025 Jun 08 17:56 | 2025 Jun 04 13:38:22 | 8.3081 | 0.00096 | 4.0695 | 300.2281 | 58.8504 | 0.98913 | 3.243 |
2025 Jun 07 17:56 | 2025 Jun 04 13:38:22 | 8.3081 | 0.00096 | 4.0695 | 300.2281 | 58.8504 | 0.98913 | 3.243 |
2025 Jun 06 17:56 | 2025 Jun 04 13:38:22 | 8.3081 | 0.00096 | 4.0695 | 300.2281 | 58.8504 | 0.98913 | 3.243 |
2025 Jun 05 17:56 | 2025 May 31 12:35:23 | 8.2986 | 0.00097 | 4.0720 | 300.4241 | 58.8504 | 0.98913 | 3.243 |
2025 Jun 04 17:57 | 2025 May 31 12:35:23 | 8.2986 | 0.00097 | 4.0720 | 300.4241 | 58.8504 | 0.98913 | 3.243 |
2025 Jun 03 17:57 | 2025 May 31 12:35:23 | 8.2986 | 0.00097 | 4.0720 | 300.4241 | 58.8504 | 0.98913 | 3.243 |