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 42206U 81053TW 22228.35097632 .00000339 00000-0 28151-3 0 9997
2 42206 82.9175 70.9502 0040933 154.7070 19.9780 13.85470888310813
Epoch (UTC): | 16 August 2022 08:25:24 |
Eccentricity: | 0.0040933 |
inclination: | 82.9175° |
perigee height: | 914 km |
apogee height: | 974 km |
right ascension of ascending node: | 70.9502° |
argument of perigee: | 154.7070° |
revolutions per day: | 13.85470888 |
mean anomaly at epoch: | 19.9780° |
orbit number at epoch: | 31081 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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