Orbital elements of CZ-3A DEB
| Launched | 1 February 2007 |
| Flight ended | – |
| Launch site | Xichang Launch Facility, PRC |
| Owner | People's Republic of China |
| NORAD ID | 35556 |
| 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 Oct 17 17:56 | 2025 Sep 28 17:27:20 | 26.0901 | 0.72376 | 23.5569 | 252.6015 | 22.3328 | 2.23355 | – |
| 2025 Oct 16 17:56 | 2025 Sep 28 17:27:20 | 26.0901 | 0.72376 | 23.5569 | 252.6015 | 22.3328 | 2.23355 | – |
| 2025 Oct 15 17:56 | 2025 Sep 28 17:27:20 | 26.0901 | 0.72376 | 23.5569 | 252.6015 | 22.3328 | 2.23355 | – |
| 2025 Oct 14 17:56 | 2025 Sep 28 17:27:20 | 26.0901 | 0.72376 | 23.5569 | 252.6015 | 22.3328 | 2.23355 | – |
| 2025 Oct 12 17:56 | 2025 Sep 28 17:27:20 | 26.0901 | 0.72376 | 23.5569 | 252.6015 | 22.3328 | 2.23355 | – |
| 2025 Oct 11 17:57 | 2025 Sep 28 17:27:20 | 26.0901 | 0.72376 | 23.5569 | 252.6015 | 22.3328 | 2.23355 | – |
| 2025 Oct 09 17:56 | 2025 Sep 28 17:27:20 | 26.0901 | 0.72376 | 23.5569 | 252.6015 | 22.3328 | 2.23355 | – |
| 2025 Oct 08 17:56 | 2025 Sep 28 17:27:20 | 26.0901 | 0.72376 | 23.5569 | 252.6015 | 22.3328 | 2.23355 | – |
| 2025 Oct 07 17:56 | 2025 Sep 28 17:27:20 | 26.0901 | 0.72376 | 23.5569 | 252.6015 | 22.3328 | 2.23355 | – |
| 2025 Oct 05 17:56 | 2025 Sep 23 19:16:42 | 26.0894 | 0.72365 | 23.6695 | 249.7424 | 22.3328 | 2.23355 | – |
| 2025 Oct 04 17:57 | 2025 Sep 23 19:16:42 | 26.0894 | 0.72365 | 23.6695 | 249.7424 | 22.3328 | 2.23355 | – |