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 21:25:04 |
| Eccentricity: | 0.0025272 |
| inclination: | 81.1459° |
| perigee height: | 476 km |
| apogee height: | 511 km |
| right ascension of ascending node: | 255.3921° |
| argument of perigee: | 347.5756° |
| revolutions per day: | 15.24036855 |
| mean anomaly at epoch: | 12.4850° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|