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 20692U 90050D 21110.00005830 0.00000250 00000-0 33376-4 0 00
2 20692 63.3181 150.9796 0893232 51.3821 308.6179 13.42256236 05
Epoch (UTC): | 20 April 2021 00:00:05 |
Eccentricity: | 0.0893232 |
inclination: | 63.3181° |
perigee height: | 433 km |
apogee height: | 1769 km |
right ascension of ascending node: | 150.9796° |
argument of perigee: | 51.3821° |
revolutions per day: | 13.42256236 |
mean anomaly at epoch: | 308.6179° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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