View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00107U 26037.10516833 +.00000000 +00000-0 +85299-3 0 00002
2 00107 28.7809 351.9447 0495894 344.4286 14.1518 14.21420135 00
| Epoch (UTC): | 06 February 2026 02:31:26 |
| Eccentricity: | 0.0495894 |
| inclination: | 28.7809° |
| perigee height: | 464 km |
| apogee height: | 1178 km |
| right ascension of ascending node: | 351.9447° |
| argument of perigee: | 344.4286° |
| revolutions per day: | 14.21420135 |
| mean anomaly at epoch: | 14.1518° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|