Orbital elements of TITAN 4 CENTAUR R/B
Launched | 7 April 2003 |
Flight ended | – |
Launch site | Air Force Eastern Test Range, Florida, USA |
Owner | United States |
NORAD ID | 27712 |
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 Jul 29 17:56 | 2025 Jul 25 09:44:10 | 10.7578 | 0.00219 | 1.6808 | 267.8477 | 91.9688 | 1.00588 | 3.243 |
2025 Jul 28 17:58 | 2025 Jul 25 09:44:10 | 10.7578 | 0.00219 | 1.6808 | 267.8477 | 91.9688 | 1.00588 | 3.243 |
2025 Jul 26 17:56 | 2025 Jul 25 09:44:10 | 10.7578 | 0.00219 | 1.6808 | 267.8477 | 91.9688 | 1.00588 | 3.243 |
2025 Jul 25 17:56 | 2025 Jul 20 10:26:27 | 10.7519 | 0.00219 | 1.6828 | 268.1063 | 91.9688 | 1.00588 | 3.243 |
2025 Jul 24 17:56 | 2025 Jul 20 10:26:27 | 10.7519 | 0.00219 | 1.6828 | 268.1063 | 91.9688 | 1.00588 | 3.243 |
2025 Jul 23 17:56 | 2025 Jul 20 10:26:27 | 10.7519 | 0.00219 | 1.6828 | 268.1063 | 91.9688 | 1.00588 | 3.243 |
2025 Jul 22 17:56 | 2025 Jul 20 10:26:27 | 10.7519 | 0.00219 | 1.6828 | 268.1063 | 91.9688 | 1.00588 | 3.243 |
2025 Jul 21 17:56 | 2025 Jul 20 10:26:27 | 10.7519 | 0.00219 | 1.6828 | 268.1063 | 91.9688 | 1.00588 | 3.243 |
2025 Jul 20 17:56 | 2025 Jul 20 10:26:27 | 10.7519 | 0.00219 | 1.6828 | 268.1063 | 91.9688 | 1.00588 | 3.243 |
2025 Jul 19 17:57 | 2025 Jul 14 11:17:36 | 10.7449 | 0.00220 | 1.6852 | 268.1743 | 91.9688 | 1.00588 | 3.243 |
2025 Jul 18 17:57 | 2025 Jul 14 11:17:36 | 10.7449 | 0.00220 | 1.6852 | 268.1743 | 91.9688 | 1.00588 | 3.243 |
2025 Jul 17 17:56 | 2025 Jul 14 11:17:36 | 10.7449 | 0.00220 | 1.6852 | 268.1743 | 91.9688 | 1.00588 | 3.243 |
2025 Jul 16 17:56 | 2025 Jul 14 11:17:36 | 10.7449 | 0.00220 | 1.6852 | 268.1743 | 91.9688 | 1.00588 | 3.243 |
2025 Jul 15 17:56 | 2025 Jul 14 11:17:36 | 10.7449 | 0.00220 | 1.6852 | 268.1743 | 91.9688 | 1.00588 | 3.243 |
2025 Jul 14 17:56 | 2025 Jul 08 12:08:38 | 10.7377 | 0.00220 | 1.6875 | 268.0787 | 91.9688 | 1.00588 | 3.243 |
2025 Jul 13 17:56 | 2025 Jul 08 12:08:38 | 10.7377 | 0.00220 | 1.6875 | 268.0787 | 91.9688 | 1.00588 | 3.243 |
2025 Jul 12 17:56 | 2025 Jul 08 12:08:38 | 10.7377 | 0.00220 | 1.6875 | 268.0787 | 91.9688 | 1.00588 | 3.243 |
2025 Jul 11 17:56 | 2025 Jul 08 12:08:38 | 10.7377 | 0.00220 | 1.6875 | 268.0787 | 91.9688 | 1.00588 | 3.243 |
2025 Jul 10 17:56 | 2025 Jul 08 12:08:38 | 10.7377 | 0.00220 | 1.6875 | 268.0787 | 91.9688 | 1.00588 | 3.243 |
2025 Jul 09 17:56 | 2025 Jul 08 12:08:38 | 10.7377 | 0.00220 | 1.6875 | 268.0787 | 91.9688 | 1.00588 | 3.243 |
2025 Jul 08 17:56 | 2025 Jul 02 12:59:52 | 10.7304 | 0.00220 | 1.6898 | 268.1668 | 91.9688 | 1.00588 | 3.243 |
2025 Jul 07 17:56 | 2025 Jul 02 12:59:52 | 10.7304 | 0.00220 | 1.6898 | 268.1668 | 91.9688 | 1.00588 | 3.243 |
2025 Jul 06 17:56 | 2025 Jul 02 12:59:52 | 10.7304 | 0.00220 | 1.6898 | 268.1668 | 91.9688 | 1.00588 | 3.243 |
2025 Jul 05 17:56 | 2025 Jul 02 12:59:52 | 10.7304 | 0.00220 | 1.6898 | 268.1668 | 91.9688 | 1.00588 | 3.243 |
2025 Jul 04 17:56 | 2025 Jul 02 12:59:52 | 10.7304 | 0.00220 | 1.6898 | 268.1668 | 91.9688 | 1.00588 | 3.243 |
2025 Jul 03 17:56 | 2025 Jul 02 12:59:52 | 10.7304 | 0.00220 | 1.6898 | 268.1668 | 91.9688 | 1.00588 | 3.243 |