View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 35869U 26032.47261405 +.00000000 +00000-0 +65980-4 0 00008
2 35869 98.7216 355.4060 0004171 350.0728 10.0367 14.23177996 03
| Epoch (UTC): | 01 February 2026 11:20:33 |
| Eccentricity: | 0.0004171 |
| inclination: | 98.7216° |
| perigee height: | 812 km |
| apogee height: | 818 km |
| right ascension of ascending node: | 355.4060° |
| argument of perigee: | 350.0728° |
| revolutions per day: | 14.23177996 |
| mean anomaly at epoch: | 10.0367° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|