View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 05435U 26159.56649204 +.00000000 +00000-0 +14708-3 0 00002
2 05435 50.1381 103.8323 0101614 145.9646 214.7857 14.60273520 09
| Epoch (UTC): | 08 June 2026 13:35:44 |
| Eccentricity: | 0.0101614 |
| inclination: | 50.1381° |
| perigee height: | 620 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 103.8323° |
| argument of perigee: | 145.9646° |
| revolutions per day: | 14.60273520 |
| mean anomaly at epoch: | 214.7857° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|