View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 05118U 26039.59701850 +.00000000 +00000-0 +39154-3 0 00008
2 05118 81.2348 87.9025 0017453 37.0608 323.1845 15.58818436 03
| Epoch (UTC): | 08 February 2026 14:19:42 |
| Eccentricity: | 0.0017453 |
| inclination: | 81.2348° |
| perigee height: | 379 km |
| apogee height: | 403 km |
| right ascension of ascending node: | 87.9025° |
| argument of perigee: | 37.0608° |
| revolutions per day: | 15.58818436 |
| mean anomaly at epoch: | 323.1845° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|