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 Apr 18 17:57 | 2025 Apr 15 23:33:40 | 41.4618 | 0.00097 | 2.6005 | 234.6211 | 125.3721 | 15.64746 | – |
| 2025 Apr 17 17:56 | 2025 Apr 15 23:33:40 | 41.4618 | 0.00097 | 2.6005 | 234.6211 | 125.3721 | 15.64746 | – |
| 2025 Apr 16 17:57 | 2025 Apr 15 23:33:40 | 41.4618 | 0.00097 | 2.6005 | 234.6211 | 125.3721 | 15.64746 | – |
| 2025 Apr 15 17:56 | 2025 Apr 09 10:19:13 | 41.4609 | 0.00077 | 5.2721 | 201.3775 | 125.3721 | 15.64746 | – |
| 2025 Apr 14 17:56 | 2025 Apr 09 10:19:13 | 41.4609 | 0.00077 | 5.2721 | 201.3775 | 125.3721 | 15.64746 | – |
| 2025 Apr 11 17:57 | 2025 Apr 09 10:19:13 | 41.4609 | 0.00077 | 5.2721 | 201.3775 | 125.3721 | 15.64746 | – |