View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 20827U 90086B 22228.11859329 .00000012 00000-0 -25883-5 0 9991
2 20827 82.5238 238.8130 0013144 17.5727 342.5885 13.83915913610427
Epoch (UTC): | 16 August 2022 02:50:46 |
Eccentricity: | 0.0013144 |
inclination: | 82.5238° |
perigee height: | 940 km |
apogee height: | 959 km |
right ascension of ascending node: | 238.8130° |
argument of perigee: | 17.5727° |
revolutions per day: | 13.83915913 |
mean anomaly at epoch: | 342.5885° |
orbit number at epoch: | 61042 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|