Orbital elements of ATLAS CENTAUR 2 DEB
Launched | 26 November 1963 |
Flight ended | – |
Launch site | Air Force Eastern Test Range, Florida, USA |
Owner | United States |
NORAD ID | 698 |
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 May 10 17:56 | 2025 May 08 11:46:18 | 29.9235 | 0.05323 | 19.7177 | 359.1706 | 0.7974 | 13.73456 | 7.743 |
2025 May 09 17:57 | 2025 May 08 11:46:18 | 29.9235 | 0.05323 | 19.7177 | 359.1706 | 0.7974 | 13.73456 | 7.743 |
2025 May 08 17:56 | 2025 May 03 14:52:25 | 29.9255 | 0.05325 | 21.4255 | 318.4667 | 0.7974 | 13.73456 | 7.743 |
2025 May 07 17:56 | 2025 May 03 14:52:25 | 29.9255 | 0.05325 | 21.4255 | 318.4667 | 0.7974 | 13.73456 | 7.743 |
2025 May 06 17:57 | 2025 May 03 14:52:25 | 29.9255 | 0.05325 | 21.4255 | 318.4667 | 0.7974 | 13.73456 | 7.743 |
2025 May 05 17:56 | 2025 May 03 14:52:25 | 29.9255 | 0.05325 | 21.4255 | 318.4667 | 0.7974 | 13.73456 | 7.743 |
2025 May 04 17:57 | 2025 May 03 14:52:25 | 29.9255 | 0.05325 | 21.4255 | 318.4667 | 0.7974 | 13.73456 | 7.743 |
2025 May 03 17:57 | 2025 May 03 14:52:25 | 29.9255 | 0.05325 | 21.4255 | 318.4667 | 0.7974 | 13.73456 | 7.743 |
2025 May 01 17:56 | 2025 Apr 21 23:45:20 | 29.9259 | 0.05325 | 1.5028 | 221.2977 | 0.7974 | 13.73456 | 7.743 |
2025 Apr 30 17:56 | 2025 Apr 21 23:45:20 | 29.9259 | 0.05325 | 1.5028 | 221.2977 | 0.7974 | 13.73456 | 7.743 |
2025 Apr 29 17:57 | 2025 Apr 21 23:45:20 | 29.9259 | 0.05325 | 1.5028 | 221.2977 | 0.7974 | 13.73456 | 7.743 |
2025 Apr 27 17:56 | 2025 Apr 21 23:45:20 | 29.9259 | 0.05325 | 1.5028 | 221.2977 | 0.7974 | 13.73456 | 7.743 |
2025 Apr 26 17:57 | 2025 Apr 21 23:45:20 | 29.9259 | 0.05325 | 1.5028 | 221.2977 | 0.7974 | 13.73456 | 7.743 |
2025 Apr 25 17:56 | 2025 Apr 21 23:45:20 | 29.9259 | 0.05325 | 1.5028 | 221.2977 | 0.7974 | 13.73456 | 7.743 |
2025 Apr 24 17:56 | 2025 Apr 21 23:45:20 | 29.9259 | 0.05325 | 1.5028 | 221.2977 | 0.7974 | 13.73456 | 7.743 |
2025 Apr 23 17:57 | 2025 Apr 21 23:45:20 | 29.9259 | 0.05325 | 1.5028 | 221.2977 | 0.7974 | 13.73456 | 7.743 |
2025 Apr 22 17:56 | 2025 Apr 21 23:45:20 | 29.9259 | 0.05325 | 1.5028 | 221.2977 | 0.7974 | 13.73456 | 7.743 |
2025 Apr 21 17:57 | 2025 Apr 15 22:59:13 | 29.9230 | 0.05325 | 3.6177 | 170.8945 | 0.7974 | 13.73456 | 7.743 |
2025 Apr 20 17:56 | 2025 Apr 15 22:59:13 | 29.9230 | 0.05325 | 3.6177 | 170.8945 | 0.7974 | 13.73456 | 7.743 |
2025 Apr 19 17:56 | 2025 Apr 15 22:59:13 | 29.9230 | 0.05325 | 3.6177 | 170.8945 | 0.7974 | 13.73456 | 7.743 |
2025 Apr 18 17:57 | 2025 Apr 15 22:59:13 | 29.9230 | 0.05325 | 3.6177 | 170.8945 | 0.7974 | 13.73456 | 7.743 |
2025 Apr 17 17:56 | 2025 Apr 15 22:59:13 | 29.9230 | 0.05325 | 3.6177 | 170.8945 | 0.7974 | 13.73456 | 7.743 |
2025 Apr 16 17:57 | 2025 Apr 15 22:59:13 | 29.9230 | 0.05325 | 3.6177 | 170.8945 | 0.7974 | 13.73456 | 7.743 |
2025 Apr 15 17:56 | 2025 Apr 10 08:40:46 | 29.9209 | 0.05325 | 5.5799 | 124.1234 | 0.7974 | 13.73456 | 7.743 |
2025 Apr 14 17:56 | 2025 Apr 10 08:40:46 | 29.9209 | 0.05325 | 5.5799 | 124.1234 | 0.7974 | 13.73456 | 7.743 |