View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63806U 26145.34157108 +.00000000 +00000-0 +57299-3 0 00008
2 63806 43.0016 99.9956 0001442 264.7704 95.2983 15.27598482 04
| Epoch (UTC): | 25 May 2026 08:11:51 |
| Eccentricity: | 0.0001442 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 99.9956° |
| argument of perigee: | 264.7704° |
| revolutions per day: | 15.27598482 |
| mean anomaly at epoch: | 95.2983° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|