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 40069U 14037A 23090.59281933 .00000110 00000-0 70082-4 0 9991
2 40069 98.4259 100.1635 0005174 196.5538 163.5466 14.20760831452631
Epoch (UTC): | 31 March 2023 14:13:39 |
Eccentricity: | 0.0005174 |
inclination: | 98.4259° |
perigee height: | 819 km |
apogee height: | 826 km |
right ascension of ascending node: | 100.1635° |
argument of perigee: | 196.5538° |
revolutions per day: | 14.20760831 |
mean anomaly at epoch: | 163.5466° |
orbit number at epoch: | 45263 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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