View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
| Epoch (UTC): | 15 January 2026 23:34:30 |
| Eccentricity: | 0.0033700 |
| inclination: | 99.1220° |
| perigee height: | 754 km |
| apogee height: | 803 km |
| right ascension of ascending node: | 26.4537° |
| argument of perigee: | 52.9609° |
| revolutions per day: | 14.33982157 |
| mean anomaly at epoch: | 307.4648° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|