View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58530U 26145.40139801 +.00000000 +00000-0 +69348-5 0 00003
2 58530 43.0057 30.1793 0001366 268.1477 91.9218 15.27582796 08
| Epoch (UTC): | 25 May 2026 09:38:00 |
| Eccentricity: | 0.0001366 |
| inclination: | 43.0057° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 30.1793° |
| argument of perigee: | 268.1477° |
| revolutions per day: | 15.27582796 |
| mean anomaly at epoch: | 91.9218° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|