View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39058U 26145.59760729 +.00000000 +00000-0 -62375-3 0 00008
2 39058 82.5003 228.9827 0017596 65.2991 294.9919 12.44024175 06
| Epoch (UTC): | 25 May 2026 14:20:33 |
| Eccentricity: | 0.0017596 |
| inclination: | 82.5003° |
| perigee height: | 1476 km |
| apogee height: | 1503 km |
| right ascension of ascending node: | 228.9827° |
| argument of perigee: | 65.2991° |
| revolutions per day: | 12.44024175 |
| mean anomaly at epoch: | 294.9919° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|