View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58529U 26145.39755154 +.00000000 +00000-0 +21488-4 0 00006
2 58529 43.0034 30.1503 0000762 268.0922 91.9843 15.27572222 00
| Epoch (UTC): | 25 May 2026 09:32:28 |
| Eccentricity: | 0.0000762 |
| inclination: | 43.0034° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 30.1503° |
| argument of perigee: | 268.0922° |
| revolutions per day: | 15.27572222 |
| mean anomaly at epoch: | 91.9843° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|