View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63788U 26145.59236845 +.00000000 +00000-0 +44181-3 0 00006
2 63788 43.0041 338.2080 0001396 261.3109 98.7585 15.27577481 00
| Epoch (UTC): | 25 May 2026 14:13:00 |
| Eccentricity: | 0.0001396 |
| inclination: | 43.0041° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 338.2080° |
| argument of perigee: | 261.3109° |
| revolutions per day: | 15.27577481 |
| mean anomaly at epoch: | 98.7585° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|