View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00082U 26140.94768593 +.00000000 +00000-0 +11954-3 0 00000
2 00082 38.8538 100.9641 1166082 94.2068 279.2443 12.27904540 06
| Epoch (UTC): | 20 May 2026 22:44:40 |
| Eccentricity: | 0.1166082 |
| inclination: | 38.8538° |
| perigee height: | 633 km |
| apogee height: | 2484 km |
| right ascension of ascending node: | 100.9641° |
| argument of perigee: | 94.2068° |
| revolutions per day: | 12.27904540 |
| mean anomaly at epoch: | 279.2443° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|