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 44744C 19074AH 21025.34029280 .00007834 00000-0 52485-3 0 251
2 44744 53.0552 338.4344 0002104 55.8015 64.2936 15.06394361 14
Epoch (UTC): | 25 January 2021 08:10:01 |
Eccentricity: | 0.0002104 |
inclination: | 53.0552° |
perigee height: | 546 km |
apogee height: | 548 km |
right ascension of ascending node: | 338.4344° |
argument of perigee: | 55.8015° |
revolutions per day: | 15.06394361 |
mean anomaly at epoch: | 64.2936° |
orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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