Orbital elements of FENGYUN 1C DEB
| Launched | 9 May 1999 |
| Flight ended | – |
| Launch site | Taiyuan Space Center, PRC |
| Owner | People's Republic of China |
| NORAD ID | 31755 |
| 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 |
| 2024 Apr 09 17:56 | 2024 Mar 31 04:53:29 | 98.7580 | 0.01923 | 6.3278 | 334.7123 | 86.7403 | 14.06638 | – |
| 2024 Apr 08 17:55 | 2024 Mar 31 04:53:29 | 98.7580 | 0.01923 | 6.3278 | 334.7123 | 86.7403 | 14.06638 | – |
| 2024 Apr 07 17:53 | 2024 Mar 31 04:53:29 | 98.7580 | 0.01923 | 6.3278 | 334.7123 | 86.7403 | 14.06638 | – |
| 2024 Apr 06 17:58 | 2024 Mar 31 04:53:29 | 98.7580 | 0.01923 | 6.3278 | 334.7123 | 86.7403 | 14.06638 | – |
| 2024 Apr 05 17:53 | 2024 Mar 31 04:53:29 | 98.7580 | 0.01923 | 6.3278 | 334.7123 | 86.7403 | 14.06638 | – |
| 2024 Apr 04 17:56 | 2024 Mar 31 04:53:29 | 98.7580 | 0.01923 | 6.3278 | 334.7123 | 86.7403 | 14.06638 | – |
| 2024 Apr 03 17:53 | 2024 Mar 31 04:53:29 | 98.7580 | 0.01923 | 6.3278 | 334.7123 | 86.7403 | 14.06638 | – |
| 2024 Apr 02 17:52 | 2024 Mar 31 04:53:29 | 98.7580 | 0.01923 | 6.3278 | 334.7123 | 86.7403 | 14.06638 | – |
| 2024 Apr 01 17:52 | 2024 Mar 31 04:53:29 | 98.7580 | 0.01923 | 6.3278 | 334.7123 | 86.7403 | 14.06638 | – |
| 2024 Mar 31 17:52 | 2024 Mar 31 04:53:29 | 98.7580 | 0.01923 | 6.3278 | 334.7123 | 86.7403 | 14.06638 | – |
| 2024 Mar 30 18:52 | 2024 Mar 23 19:37:55 | 98.7570 | 0.01928 | 5.8507 | 355.5259 | 86.7403 | 14.06638 | – |
| 2024 Mar 29 18:52 | 2024 Mar 23 19:37:55 | 98.7570 | 0.01928 | 5.8507 | 355.5259 | 86.7403 | 14.06638 | – |
| 2024 Mar 28 18:52 | 2024 Mar 23 19:37:55 | 98.7570 | 0.01928 | 5.8507 | 355.5259 | 86.7403 | 14.06638 | – |
| 2024 Mar 27 18:52 | 2024 Mar 23 19:37:55 | 98.7570 | 0.01928 | 5.8507 | 355.5259 | 86.7403 | 14.06638 | – |