View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 31598U 26020.31646095 +.00000000 +00000-0 +90643-3 0 00008
2 31598 97.8832 210.9787 0000954 82.7677 277.3652 14.96093150 04
| Epoch (UTC): | 20 January 2026 07:35:42 |
| Eccentricity: | 0.0000954 |
| inclination: | 97.8832° |
| perigee height: | 578 km |
| apogee height: | 580 km |
| right ascension of ascending node: | 210.9787° |
| argument of perigee: | 82.7677° |
| revolutions per day: | 14.96093150 |
| mean anomaly at epoch: | 277.3652° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|