View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58405U 26145.57700994 +.00000000 +00000-0 +10589-4 0 00001
2 58405 43.0012 338.4464 0000956 279.5349 80.5395 15.27580718 09
| Epoch (UTC): | 25 May 2026 13:50:53 |
| Eccentricity: | 0.0000956 |
| inclination: | 43.0012° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 338.4464° |
| argument of perigee: | 279.5349° |
| revolutions per day: | 15.27580718 |
| mean anomaly at epoch: | 80.5395° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|