View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 116U 61015A 22146.86715386 .00000030 00000-0 82017-4 0 9995
2 116 66.8099 276.3487 0081337 235.4679 123.8704 13.91829826 90882
| Epoch (UTC): | 26 May 2022 20:48:42 |
| Eccentricity: | 0.0081337 |
| inclination: | 66.8099° |
| perigee height: | 863 km |
| apogee height: | 981 km |
| right ascension of ascending node: | 276.3487° |
| argument of perigee: | 235.4679° |
| revolutions per day: | 13.91829826 |
| mean anomaly at epoch: | 123.8704° |
| orbit number at epoch: | 9088 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|