View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 24278U 26073.60013970 +.00000000 +00000-0 +60160-4 0 00007
2 24278 98.5375 295.3553 0349616 342.0303 16.8727 13.53269068 02
| Epoch (UTC): | 14 March 2026 14:24:12 |
| Eccentricity: | 0.0349616 |
| inclination: | 98.5375° |
| perigee height: | 800 km |
| apogee height: | 1320 km |
| right ascension of ascending node: | 295.3553° |
| argument of perigee: | 342.0303° |
| revolutions per day: | 13.53269068 |
| mean anomaly at epoch: | 16.8727° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|