View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 30342U 99025ABD 22181.45601793 .00000208 00000-0 23181-3 0 9994
2 30342 100.1264 257.9064 0175470 119.9755 8.7095 13.77082902775122
Epoch (UTC): | 30 June 2022 10:56:39 |
Eccentricity: | 0.0175470 |
inclination: | 100.1264° |
perigee height: | 845 km |
apogee height: | 1103 km |
right ascension of ascending node: | 257.9064° |
argument of perigee: | 119.9755° |
revolutions per day: | 13.77082902 |
mean anomaly at epoch: | 8.7095° |
orbit number at epoch: | 77512 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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