View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 49585U 82092CA 21359.64652454 .11849952 -93538-6 38370-2 0 9995
2 49585 82.1994 77.6852 0030431 25.7687 334.5111 16.24789592 6059
| Epoch (UTC): | 25 December 2021 15:30:59 |
| Eccentricity: | 0.0030431 |
| inclination: | 82.1994° |
| perigee height: | 186 km |
| apogee height: | 226 km |
| right ascension of ascending node: | 77.6852° |
| argument of perigee: | 25.7687° |
| revolutions per day: | 16.24789592 |
| mean anomaly at epoch: | 334.5111° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|