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 44080U 19018C 21023.69622678 .00002241 00000-0 95361-4 0 9996
2 44080 97.3825 87.0718 0014022 108.8111 251.4649 15.23964434100926
Epoch (UTC): | 23 January 2021 16:42:33 |
Eccentricity: | 0.0014022 |
inclination: | 97.3825° |
perigee height: | 484 km |
apogee height: | 503 km |
right ascension of ascending node: | 87.0718° |
argument of perigee: | 108.8111° |
revolutions per day: | 15.23964434 |
mean anomaly at epoch: | 251.4649° |
orbit number at epoch: | 10092 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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