View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58420U 26145.54487950 +.00000000 +00000-0 +69743-4 0 00005
2 58420 43.0024 338.1973 0001542 265.9174 94.1501 15.27580986 05
| Epoch (UTC): | 25 May 2026 13:04:37 |
| Eccentricity: | 0.0001542 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 338.1973° |
| argument of perigee: | 265.9174° |
| revolutions per day: | 15.27580986 |
| mean anomaly at epoch: | 94.1501° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|