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 44420U 19036AC 19344.99573134 .00004307 00000-0 95226-3 0 9996
2 44420 24.0060 223.2023 0023437 225.4347 134.3875 14.53864598 22691
Epoch (UTC): | 10 December 2019 23:53:51 |
Eccentricity: | 0.0023437 |
inclination: | 24.0060° |
perigee height: | 696 km |
apogee height: | 729 km |
right ascension of ascending node: | 223.2023° |
argument of perigee: | 225.4347° |
revolutions per day: | 14.53864598 |
mean anomaly at epoch: | 134.3875° |
orbit number at epoch: | 2269 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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