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 Nov 15 18:57 | 2025 Nov 08 18:47:45 | 10.8917 | 0.00239 | 1.6398 | 268.7833 | 90.8851 | 1.00595 | 3.243 |
| 2025 Nov 13 18:56 | 2025 Nov 08 18:47:45 | 10.8917 | 0.00239 | 1.6398 | 268.7833 | 90.8851 | 1.00595 | 3.243 |
| 2025 Nov 12 18:57 | 2025 Nov 08 18:47:45 | 10.8917 | 0.00239 | 1.6398 | 268.7833 | 90.8851 | 1.00595 | 3.243 |
| 2025 Nov 11 18:55 | 2025 Nov 08 18:47:45 | 10.8917 | 0.00239 | 1.6398 | 268.7833 | 90.8851 | 1.00595 | 3.243 |
| 2025 Nov 10 18:57 | 2025 Nov 08 18:47:45 | 10.8917 | 0.00239 | 1.6398 | 268.7833 | 90.8851 | 1.00595 | 3.243 |
| 2025 Nov 09 18:57 | 2025 Nov 08 18:47:45 | 10.8917 | 0.00239 | 1.6398 | 268.7833 | 90.8851 | 1.00595 | 3.243 |
| 2025 Nov 08 18:56 | 2025 Oct 31 19:56:15 | 10.8822 | 0.00238 | 1.6429 | 268.3556 | 90.8851 | 1.00595 | 3.243 |
| 2025 Nov 07 18:57 | 2025 Oct 31 19:56:15 | 10.8822 | 0.00238 | 1.6429 | 268.3556 | 90.8851 | 1.00595 | 3.243 |
| 2025 Nov 05 18:57 | 2025 Oct 31 19:56:15 | 10.8822 | 0.00238 | 1.6429 | 268.3556 | 90.8851 | 1.00595 | 3.243 |
| 2025 Nov 04 18:57 | 2025 Oct 31 19:56:15 | 10.8822 | 0.00238 | 1.6429 | 268.3556 | 90.8851 | 1.00595 | 3.243 |
| 2025 Nov 03 18:57 | 2025 Oct 31 19:56:15 | 10.8822 | 0.00238 | 1.6429 | 268.3556 | 90.8851 | 1.00595 | 3.243 |
| 2025 Nov 02 18:57 | 2025 Oct 26 20:38:43 | 10.8760 | 0.00237 | 1.6447 | 268.0449 | 90.8851 | 1.00595 | 3.243 |
| 2025 Nov 01 18:58 | 2025 Oct 26 20:38:43 | 10.8760 | 0.00237 | 1.6447 | 268.0449 | 90.8851 | 1.00595 | 3.243 |
| 2025 Oct 31 18:57 | 2025 Oct 26 20:38:43 | 10.8760 | 0.00237 | 1.6447 | 268.0449 | 90.8851 | 1.00595 | 3.243 |
| 2025 Oct 30 18:57 | 2025 Oct 26 20:38:43 | 10.8760 | 0.00237 | 1.6447 | 268.0449 | 90.8851 | 1.00595 | 3.243 |
| 2025 Oct 29 18:57 | 2025 Oct 26 20:38:43 | 10.8760 | 0.00237 | 1.6447 | 268.0449 | 90.8851 | 1.00595 | 3.243 |
| 2025 Oct 28 18:57 | 2025 Oct 22 21:12:33 | 10.8709 | 0.00237 | 1.6462 | 267.7822 | 90.8851 | 1.00595 | 3.243 |
| 2025 Oct 27 18:57 | 2025 Oct 22 21:12:33 | 10.8709 | 0.00237 | 1.6462 | 267.7822 | 90.8851 | 1.00595 | 3.243 |
| 2025 Oct 26 18:57 | 2025 Oct 22 21:12:33 | 10.8709 | 0.00237 | 1.6462 | 267.7822 | 90.8851 | 1.00595 | 3.243 |
| 2025 Oct 25 17:57 | 2025 Oct 22 21:12:33 | 10.8709 | 0.00237 | 1.6462 | 267.7822 | 90.8851 | 1.00595 | 3.243 |
| 2025 Oct 24 17:57 | 2025 Oct 22 21:12:33 | 10.8709 | 0.00237 | 1.6462 | 267.7822 | 90.8851 | 1.00595 | 3.243 |
| 2025 Oct 22 17:56 | 2025 Oct 17 21:54:51 | 10.8643 | 0.00234 | 1.6479 | 267.6758 | 90.8851 | 1.00595 | 3.243 |
| 2025 Oct 21 17:56 | 2025 Oct 17 21:54:51 | 10.8643 | 0.00234 | 1.6479 | 267.6758 | 90.8851 | 1.00595 | 3.243 |
| 2025 Oct 20 17:56 | 2025 Oct 17 21:54:51 | 10.8643 | 0.00234 | 1.6479 | 267.6758 | 90.8851 | 1.00595 | 3.243 |
| 2025 Oct 19 17:56 | 2025 Oct 17 21:54:51 | 10.8643 | 0.00234 | 1.6479 | 267.6758 | 90.8851 | 1.00595 | 3.243 |