View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63791U 26145.55268196 +.00000000 +00000-0 +66953-3 0 00001
2 63791 42.9995 338.7725 0001254 275.8632 84.2077 15.27572888 07
| Epoch (UTC): | 25 May 2026 13:15:51 |
| Eccentricity: | 0.0001254 |
| inclination: | 42.9995° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 338.7725° |
| argument of perigee: | 275.8632° |
| revolutions per day: | 15.27572888 |
| mean anomaly at epoch: | 84.2077° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|