View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 45875U 20046C 23069.83120406 0.00085000 00000-0 36277-2 0 08
2 45875 53.9765 20.1247 0005409 48.4274 311.5725 15.22388742 05
| Epoch (UTC): | 10 March 2023 19:56:56 |
| Eccentricity: | 0.0005409 |
| inclination: | 53.9765° |
| perigee height: | 495 km |
| apogee height: | 502 km |
| right ascension of ascending node: | 20.1247° |
| argument of perigee: | 48.4274° |
| revolutions per day: | 15.22388742 |
| mean anomaly at epoch: | 311.5725° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|