View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00047U 60007C 23333.52048953 .00000735 00000-0 18862-3 0 9997
2 00047 66.6671 24.0975 0217309 101.4286 261.1312 14.43177711316402
Epoch (UTC): | 29 November 2023 12:29:30 |
Eccentricity: | 0.0217309 |
inclination: | 66.6671° |
perigee height: | 593 km |
apogee height: | 903 km |
right ascension of ascending node: | 24.0975° |
argument of perigee: | 101.4286° |
revolutions per day: | 14.43177711 |
mean anomaly at epoch: | 261.1312° |
orbit number at epoch: | 31640 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|