View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63025U 26145.58515628 +.00000000 +00000-0 +10096-2 0 00005
2 63025 43.0009 261.4799 0001900 277.1046 82.9589 15.27626392 03
| Epoch (UTC): | 25 May 2026 14:02:37 |
| Eccentricity: | 0.0001900 |
| inclination: | 43.0009° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 261.4799° |
| argument of perigee: | 277.1046° |
| revolutions per day: | 15.27626392 |
| mean anomaly at epoch: | 82.9589° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|