View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 31598U 26041.91753083 +.00000000 +00000-0 +32803-3 0 00007
2 31598 97.8859 232.7396 0000860 86.6287 273.5032 14.96318751 04
| Epoch (UTC): | 10 February 2026 22:01:14 |
| Eccentricity: | 0.0000860 |
| inclination: | 97.8859° |
| perigee height: | 578 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 232.7396° |
| argument of perigee: | 86.6287° |
| revolutions per day: | 14.96318751 |
| mean anomaly at epoch: | 273.5032° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|