View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 31598U 26049.87513784 +.00000000 +00000-0 +33004-3 0 00006
2 31598 97.8862 240.7584 0001438 92.1173 268.0213 14.96380727 06
| Epoch (UTC): | 18 February 2026 21:00:11 |
| Eccentricity: | 0.0001438 |
| inclination: | 97.8862° |
| perigee height: | 577 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 240.7584° |
| argument of perigee: | 92.1173° |
| revolutions per day: | 14.96380727 |
| mean anomaly at epoch: | 268.0213° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|