View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62289U 26145.47845304 +.00000000 +00000-0 +74213-3 0 00003
2 62289 43.0018 142.8808 0001775 260.6296 99.4355 15.27580094 03
| Epoch (UTC): | 25 May 2026 11:28:58 |
| Eccentricity: | 0.0001775 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 142.8808° |
| argument of perigee: | 260.6296° |
| revolutions per day: | 15.27580094 |
| mean anomaly at epoch: | 99.4355° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|