Orbital elements of CZ-3A R/B
| Launched | 1 February 2007 |
| Flight ended | – |
| Launch site | Xichang Launch Facility, PRC |
| Owner | People's Republic of China |
| NORAD ID | 30324 |
| 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 |
| 2026 Feb 05 18:58 | 2026 Feb 01 19:54:17 | 24.6533 | 0.57714 | 6.6448 | 270.0781 | 27.7002 | 4.37196 | – |
| 2026 Feb 04 18:57 | 2026 Feb 01 19:54:17 | 24.6533 | 0.57714 | 6.6448 | 270.0781 | 27.7002 | 4.37196 | – |
| 2026 Feb 03 18:56 | 2026 Feb 01 19:54:17 | 24.6533 | 0.57714 | 6.6448 | 270.0781 | 27.7002 | 4.37196 | – |
| 2026 Feb 02 18:56 | 2026 Feb 01 19:54:17 | 24.6533 | 0.57714 | 6.6448 | 270.0781 | 27.7002 | 4.37196 | – |
| 2026 Feb 01 18:56 | 2026 Jan 27 13:42:29 | 24.6496 | 0.57705 | 6.9438 | 262.3605 | 27.7002 | 4.37196 | – |
| 2026 Jan 31 18:56 | 2026 Jan 27 13:42:29 | 24.6496 | 0.57705 | 6.9438 | 262.3605 | 27.7002 | 4.37196 | – |
| 2026 Jan 30 18:57 | 2026 Jan 27 13:42:29 | 24.6496 | 0.57705 | 6.9438 | 262.3605 | 27.7002 | 4.37196 | – |
| 2026 Jan 29 18:56 | 2026 Jan 27 13:42:29 | 24.6496 | 0.57705 | 6.9438 | 262.3605 | 27.7002 | 4.37196 | – |
| 2026 Jan 28 18:56 | 2026 Jan 27 13:42:29 | 24.6496 | 0.57705 | 6.9438 | 262.3605 | 27.7002 | 4.37196 | – |
| 2026 Jan 27 18:56 | 2026 Jan 21 09:33:40 | 24.6452 | 0.57695 | 7.2945 | 253.3022 | 27.7002 | 4.37196 | – |
| 2026 Jan 26 18:57 | 2026 Jan 21 09:33:40 | 24.6452 | 0.57695 | 7.2945 | 253.3022 | 27.7002 | 4.37196 | – |
| 2026 Jan 25 18:57 | 2026 Jan 21 09:33:40 | 24.6452 | 0.57695 | 7.2945 | 253.3022 | 27.7002 | 4.37196 | – |
| 2026 Jan 24 18:58 | 2026 Jan 21 09:33:40 | 24.6452 | 0.57695 | 7.2945 | 253.3022 | 27.7002 | 4.37196 | – |