View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 20578U 26066.34286823 +.00000000 +00000-0 +89402-4 0 00008
2 20578 82.9469 154.9808 0014161 73.1279 353.3348 13.76636453 02
| Epoch (UTC): | 07 March 2026 08:13:43 |
| Eccentricity: | 0.0014161 |
| inclination: | 82.9469° |
| perigee height: | 965 km |
| apogee height: | 986 km |
| right ascension of ascending node: | 154.9808° |
| argument of perigee: | 73.1279° |
| revolutions per day: | 13.76636453 |
| mean anomaly at epoch: | 353.3348° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|