View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58692U 26145.57243252 +.00000000 +00000-0 +42141-4 0 00007
2 58692 49.9979 66.9587 0001314 28.8104 331.2846 13.41457053 02
| Epoch (UTC): | 25 May 2026 13:44:18 |
| Eccentricity: | 0.0001314 |
| inclination: | 49.9979° |
| perigee height: | 1103 km |
| apogee height: | 1105 km |
| right ascension of ascending node: | 66.9587° |
| argument of perigee: | 28.8104° |
| revolutions per day: | 13.41457053 |
| mean anomaly at epoch: | 331.2846° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|