View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00051U 60009C 23037.87082634 .00000006 00000-0 88497-3 0 9999
2 00051 47.2099 243.7420 0107750 149.2265 211.4898 12.18292876781667
Epoch (UTC): | 06 February 2023 20:53:59 |
Eccentricity: | 0.0107750 |
inclination: | 47.2099° |
perigee height: | 1514 km |
apogee height: | 1686 km |
right ascension of ascending node: | 243.7420° |
argument of perigee: | 149.2265° |
revolutions per day: | 12.18292876 |
mean anomaly at epoch: | 211.4898° |
orbit number at epoch: | 78166 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|