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 43941U 19004A 21100.12230554 0.00000000 00000-0 00000-0 0 04
2 43941 73.5818 81.3777 0010525 267.7546 92.2454 15.52996450 00
Epoch (UTC): | 10 April 2021 02:56:07 |
Eccentricity: | 0.0010525 |
inclination: | 73.5818° |
perigee height: | 401 km |
apogee height: | 415 km |
right ascension of ascending node: | 81.3777° |
argument of perigee: | 267.7546° |
revolutions per day: | 15.52996450 |
mean anomaly at epoch: | 92.2454° |
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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