View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58389U 26145.60242909 +.00000000 +00000-0 +42632-4 0 00007
2 58389 53.1607 4.0628 0001143 90.3320 269.7812 15.30201716 04
| Epoch (UTC): | 25 May 2026 14:27:29 |
| Eccentricity: | 0.0001143 |
| inclination: | 53.1607° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 4.0628° |
| argument of perigee: | 90.3320° |
| revolutions per day: | 15.30201716 |
| mean anomaly at epoch: | 269.7812° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|