View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00116U 61015A 22022.55190568 -.00000047 00000-0 22993-4 0 9999
2 00116 66.8077 220.2861 0080274 316.0947 43.3771 13.91808880 73085
| Epoch (UTC): | 22 January 2022 13:14:44 |
| Eccentricity: | 0.0080274 |
| inclination: | 66.8077° |
| perigee height: | 863 km |
| apogee height: | 981 km |
| right ascension of ascending node: | 220.2861° |
| argument of perigee: | 316.0947° |
| revolutions per day: | 13.91808880 |
| mean anomaly at epoch: | 43.3771° |
| orbit number at epoch: | 7308 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|