View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56163U 26100.14300654 +.00000000 +00000-0 +63540-4 0 00008
2 56163 80.9992 136.8356 0007293 136.7690 223.4039 13.84973150 09
| Epoch (UTC): | 10 April 2026 03:25:55 |
| Eccentricity: | 0.0007293 |
| inclination: | 80.9992° |
| perigee height: | 941 km |
| apogee height: | 952 km |
| right ascension of ascending node: | 136.8356° |
| argument of perigee: | 136.7690° |
| revolutions per day: | 13.84973150 |
| mean anomaly at epoch: | 223.4039° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|