View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43871U 26145.59111720 +.00000000 +00000-0 +12061-3 0 00003
2 43871 99.7563 167.8088 0014615 109.9613 250.3098 13.51209929 06
| Epoch (UTC): | 25 May 2026 14:11:12 |
| Eccentricity: | 0.0014615 |
| inclination: | 99.7563° |
| perigee height: | 1057 km |
| apogee height: | 1079 km |
| right ascension of ascending node: | 167.8088° |
| argument of perigee: | 109.9613° |
| revolutions per day: | 13.51209929 |
| mean anomaly at epoch: | 250.3098° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|