View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58076U 26145.30840554 +.00000000 +00000-0 -51123-5 0 00004
2 58076 43.0058 5.1775 0001103 278.1393 81.9333 15.27584087 05
| Epoch (UTC): | 25 May 2026 07:24:06 |
| Eccentricity: | 0.0001103 |
| inclination: | 43.0058° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 5.1775° |
| argument of perigee: | 278.1393° |
| revolutions per day: | 15.27584087 |
| mean anomaly at epoch: | 81.9333° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|