View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58835U 26145.34427714 +.00000000 +00000-0 +16257-3 0 00006
2 58835 53.1604 208.1719 0000803 222.9159 137.1779 15.30203881 05
| Epoch (UTC): | 25 May 2026 08:15:45 |
| Eccentricity: | 0.0000803 |
| inclination: | 53.1604° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 208.1719° |
| argument of perigee: | 222.9159° |
| revolutions per day: | 15.30203881 |
| mean anomaly at epoch: | 137.1779° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|