View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 31792U 26100.46324661 +.00000000 +00000-0 -26330-4 0 00005
2 31792 70.9410 136.6557 0009637 243.6889 116.3243 14.12948775 01
| Epoch (UTC): | 10 April 2026 11:07:04 |
| Eccentricity: | 0.0009637 |
| inclination: | 70.9410° |
| perigee height: | 842 km |
| apogee height: | 856 km |
| right ascension of ascending node: | 136.6557° |
| argument of perigee: | 243.6889° |
| revolutions per day: | 14.12948775 |
| mean anomaly at epoch: | 116.3243° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|