Orbital elements of OBJECT E
| Launched | 28 April 2021 |
| Flight ended | – |
| Launch site | Wenchang Satellite Launch Center, PRC |
| Owner | People's Republic of China |
| NORAD ID | 63523 |
| 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 Oct 01 19:24:24 | 41.4575 | 0.00105 | 5.2128 | 303.7341 | 56.2500 | 15.69879 | – |
| 2025 Oct 16 17:56 | 2025 Oct 01 19:24:24 | 41.4575 | 0.00105 | 5.2128 | 303.7341 | 56.2500 | 15.69879 | – |
| 2025 Oct 15 17:56 | 2025 Oct 01 19:24:24 | 41.4575 | 0.00105 | 5.2128 | 303.7341 | 56.2500 | 15.69879 | – |
| 2025 Oct 14 17:56 | 2025 Oct 01 19:24:24 | 41.4575 | 0.00105 | 5.2128 | 303.7341 | 56.2500 | 15.69879 | – |
| 2025 Oct 12 17:56 | 2025 Oct 01 19:24:24 | 41.4575 | 0.00105 | 5.2128 | 303.7341 | 56.2500 | 15.69879 | – |
| 2025 Oct 11 17:57 | 2025 Oct 01 19:24:24 | 41.4575 | 0.00105 | 5.2128 | 303.7341 | 56.2500 | 15.69879 | – |
| 2025 Oct 09 17:56 | 2025 Oct 01 19:24:24 | 41.4575 | 0.00105 | 5.2128 | 303.7341 | 56.2500 | 15.69879 | – |
| 2025 Oct 08 17:56 | 2025 Oct 01 19:24:24 | 41.4575 | 0.00105 | 5.2128 | 303.7341 | 56.2500 | 15.69879 | – |
| 2025 Oct 07 17:56 | 2025 Oct 01 19:24:24 | 41.4575 | 0.00105 | 5.2128 | 303.7341 | 56.2500 | 15.69879 | – |
| 2025 Sep 25 17:56 | 2025 Sep 09 07:37:51 | 41.4571 | 0.00157 | 14.4917 | 189.8893 | 56.2500 | 15.69879 | – |
| 2025 Sep 24 17:56 | 2025 Sep 09 07:37:51 | 41.4571 | 0.00157 | 14.4917 | 189.8893 | 56.2500 | 15.69879 | – |