View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43770U 26111.42536778 +.00000000 +00000-0 +42708-3 0 00001
2 43770 97.4422 171.9227 0009258 177.8365 182.2915 15.25462386 01
| Epoch (UTC): | 21 April 2026 10:12:31 |
| Eccentricity: | 0.0009258 |
| inclination: | 97.4422° |
| perigee height: | 483 km |
| apogee height: | 496 km |
| right ascension of ascending node: | 171.9227° |
| argument of perigee: | 177.8365° |
| revolutions per day: | 15.25462386 |
| mean anomaly at epoch: | 182.2915° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|