View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 44879U 19093A 22176.86787914 .00001304 00000-0 16955-3 0 9999
2 44879 97.8956 256.2726 0016010 151.7092 208.4968 14.82290264136040
Epoch (UTC): | 25 June 2022 20:49:44 |
Eccentricity: | 0.0016010 |
inclination: | 97.8956° |
perigee height: | 611 km |
apogee height: | 633 km |
right ascension of ascending node: | 256.2726° |
argument of perigee: | 151.7092° |
revolutions per day: | 14.82290264 |
mean anomaly at epoch: | 208.4968° |
orbit number at epoch: | 13604 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|