View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64930U 26145.26575166 +.00000000 +00000-0 +56760-3 0 00008
2 64930 53.1591 349.5606 0000894 68.0649 292.0447 15.31720868 04
| Epoch (UTC): | 25 May 2026 06:22:40 |
| Eccentricity: | 0.0000894 |
| inclination: | 53.1591° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 349.5606° |
| argument of perigee: | 68.0649° |
| revolutions per day: | 15.31720868 |
| mean anomaly at epoch: | 292.0447° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|