View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 31797U 26145.59788781 +.00000000 +00000-0 +61462-3 0 00003
2 31797 98.1016 247.3025 0012520 183.9058 176.2094 15.46657612 03
| Epoch (UTC): | 25 May 2026 14:20:57 |
| Eccentricity: | 0.0012520 |
| inclination: | 98.1016° |
| perigee height: | 418 km |
| apogee height: | 435 km |
| right ascension of ascending node: | 247.3025° |
| argument of perigee: | 183.9058° |
| revolutions per day: | 15.46657612 |
| mean anomaly at epoch: | 176.2094° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|