View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 31598U 26070.26916409 +.00000000 +00000-0 +37795-3 0 00005
2 31598 97.8876 261.3134 0001393 99.5754 260.5625 14.96549270 01
| Epoch (UTC): | 11 March 2026 06:27:35 |
| Eccentricity: | 0.0001393 |
| inclination: | 97.8876° |
| perigee height: | 577 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 261.3134° |
| argument of perigee: | 99.5754° |
| revolutions per day: | 14.96549270 |
| mean anomaly at epoch: | 260.5625° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|