View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 25338U 26073.60649720 +.00000000 +00000-0 +88795-4 0 00007
2 25338 98.5158 96.7593 0009066 263.8212 96.1936 14.27114805 00
| Epoch (UTC): | 14 March 2026 14:33:21 |
| Eccentricity: | 0.0009066 |
| inclination: | 98.5158° |
| perigee height: | 795 km |
| apogee height: | 808 km |
| right ascension of ascending node: | 96.7593° |
| argument of perigee: | 263.8212° |
| revolutions per day: | 14.27114805 |
| mean anomaly at epoch: | 96.1936° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|