View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00022U 59009A 23160.91633703 .00007733 00000-0 52760-3 0 9994
2 00022 50.2814 27.9368 0126503 103.5050 258.0030 15.00787883633234
Epoch (UTC): | 09 June 2023 21:59:31 |
Eccentricity: | 0.0126503 |
inclination: | 50.2814° |
perigee height: | 476 km |
apogee height: | 652 km |
right ascension of ascending node: | 27.9368° |
argument of perigee: | 103.5050° |
revolutions per day: | 15.00787883 |
mean anomaly at epoch: | 258.0030° |
orbit number at epoch: | 63323 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|