View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
| Epoch (UTC): | 14 January 2026 12:52:18 |
| Eccentricity: | 0.0015966 |
| inclination: | 97.7461° |
| perigee height: | 498 km |
| apogee height: | 520 km |
| right ascension of ascending node: | 40.6575° |
| argument of perigee: | 200.0868° |
| revolutions per day: | 15.18829111 |
| mean anomaly at epoch: | 159.9740° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|