View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 38101U 26107.01610145 +.00000000 +00000-0 +00000-0 0 00000
2 38101 8.7124 56.9485 0006156 247.6362 292.5764 1.00358332 02
| Epoch (UTC): | 17 April 2026 00:23:11 |
| Eccentricity: | 0.0006156 |
| inclination: | 8.7124° |
| perigee height: | 35736 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 56.9485° |
| argument of perigee: | 247.6362° |
| revolutions per day: | 1.00358332 |
| mean anomaly at epoch: | 292.5764° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|