View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 48274U 21035A 22176.47654722 .00012192 00000-0 14746-3 0 9991
2 48274 41.4701 168.5170 0003574 324.4979 174.1983 15.60516824 66068
Epoch (UTC): | 25 June 2022 11:26:13 |
Eccentricity: | 0.0003574 |
inclination: | 41.4701° |
perigee height: | 384 km |
apogee height: | 388 km |
right ascension of ascending node: | 168.5170° |
argument of perigee: | 324.4979° |
revolutions per day: | 15.60516824 |
mean anomaly at epoch: | 174.1983° |
orbit number at epoch: | 6606 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|