Orbital elements of FENGYUN 4A
| Launched | 9 December 2016 |
| Flight ended | – |
| Launch site | Xichang Launch Facility, PRC |
| Owner | People's Republic of China |
| NORAD ID | 41882 |
| 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 05 12:36:24 | 1.9879 | 0.00064 | 5.4531 | 133.4809 | 233.1608 | 1.00277 | – |
| 2026 Feb 04 18:57 | 2026 Feb 04 08:50:02 | 1.9847 | 0.00065 | 5.4534 | 133.8121 | 233.1608 | 1.00277 | – |
| 2026 Feb 03 18:56 | 2026 Feb 03 10:34:47 | 1.9822 | 0.00065 | 5.4541 | 133.8645 | 233.1608 | 1.00277 | – |
| 2026 Feb 02 18:56 | 2026 Feb 02 12:19:39 | 1.9794 | 0.00065 | 5.4548 | 133.8563 | 233.1608 | 1.00277 | – |
| 2026 Feb 01 18:56 | 2026 Feb 01 12:21:45 | 1.9764 | 0.00066 | 5.4555 | 133.8184 | 233.1608 | 1.00277 | – |
| 2026 Jan 31 18:56 | 2026 Jan 31 12:23:49 | 1.9734 | 0.00066 | 5.4564 | 133.8118 | 233.1608 | 1.00277 | – |
| 2026 Jan 30 18:57 | 2026 Jan 30 14:08:40 | 1.9718 | 0.00065 | 5.4575 | 133.7602 | 233.1608 | 1.00277 | – |
| 2026 Jan 29 18:56 | 2026 Jan 29 10:45:23 | 1.9677 | 0.00054 | 5.4588 | 137.5014 | 233.1608 | 1.00277 | – |
| 2026 Jan 28 18:56 | 2026 Jan 27 21:05:50 | 1.9635 | 0.00053 | 5.4604 | 136.8464 | 233.1608 | 1.00277 | – |
| 2026 Jan 27 18:56 | 2026 Jan 27 12:32:15 | 1.9626 | 0.00054 | 5.4608 | 136.3406 | 233.1608 | 1.00277 | – |
| 2026 Jan 26 18:57 | 2026 Jan 26 13:28:37 | 1.9601 | 0.00053 | 5.4617 | 135.6007 | 233.1608 | 1.00277 | – |
| 2026 Jan 25 18:57 | 2026 Jan 25 12:36:31 | 1.9575 | 0.00053 | 5.4625 | 134.7376 | 233.1608 | 1.00277 | – |
| 2026 Jan 24 18:58 | 2026 Jan 24 12:38:40 | 1.9550 | 0.00052 | 5.4633 | 134.0522 | 233.1608 | 1.00277 | – |