View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58492U 26145.62308212 +.00000000 +00000-0 +16281-4 0 00005
2 58492 43.0032 349.0412 0001292 260.4612 99.6094 15.27576227 01
| Epoch (UTC): | 25 May 2026 14:57:14 |
| Eccentricity: | 0.0001292 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 349.0412° |
| argument of perigee: | 260.4612° |
| revolutions per day: | 15.27576227 |
| mean anomaly at epoch: | 99.6094° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|