View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 28096U 26065.01744250 +.00000000 +00000-0 +96062-4 0 00007
2 28096 63.6796 295.5969 0073455 118.0137 242.8346 13.41062509 04
| Epoch (UTC): | 06 March 2026 00:25:07 |
| Eccentricity: | 0.0073455 |
| inclination: | 63.6796° |
| perigee height: | 1050 km |
| apogee height: | 1160 km |
| right ascension of ascending node: | 295.5969° |
| argument of perigee: | 118.0137° |
| revolutions per day: | 13.41062509 |
| mean anomaly at epoch: | 242.8346° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|