View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 24305U 26039.12568883 +.00000000 +00000-0 +77194-4 0 00000
2 24305 82.9394 175.7272 0028963 250.2054 109.5978 13.74070811 09
| Epoch (UTC): | 08 February 2026 03:00:59 |
| Eccentricity: | 0.0028963 |
| inclination: | 82.9394° |
| perigee height: | 964 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 175.7272° |
| argument of perigee: | 250.2054° |
| revolutions per day: | 13.74070811 |
| mean anomaly at epoch: | 109.5978° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|