View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 24903U 26100.11379647 +.00000000 +00000-0 +10208-3 0 00002
2 24903 86.3993 345.8291 0002150 92.2135 267.9309 14.37444989 09
| Epoch (UTC): | 10 April 2026 02:43:52 |
| Eccentricity: | 0.0002150 |
| inclination: | 86.3993° |
| perigee height: | 765 km |
| apogee height: | 768 km |
| right ascension of ascending node: | 345.8291° |
| argument of perigee: | 92.2135° |
| revolutions per day: | 14.37444989 |
| mean anomaly at epoch: | 267.9309° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|