View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00107U 26140.23603850 +.00000000 +00000-0 +11967-3 0 00008
2 00107 28.7794 117.5909 0493976 227.2571 128.5406 14.22000795 09
| Epoch (UTC): | 20 May 2026 05:39:53 |
| Eccentricity: | 0.0493976 |
| inclination: | 28.7794° |
| perigee height: | 463 km |
| apogee height: | 1174 km |
| right ascension of ascending node: | 117.5909° |
| argument of perigee: | 227.2571° |
| revolutions per day: | 14.22000795 |
| mean anomaly at epoch: | 128.5406° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|