View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58983U 26145.39643310 +.00000000 +00000-0 +47006-4 0 00004
2 58983 53.1612 299.9486 0001103 98.6860 261.4268 15.34395489 02
| Epoch (UTC): | 25 May 2026 09:30:51 |
| Eccentricity: | 0.0001103 |
| inclination: | 53.1612° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 299.9486° |
| argument of perigee: | 98.6860° |
| revolutions per day: | 15.34395489 |
| mean anomaly at epoch: | 261.4268° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|