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 00012U 59001B 21026.73505830 .00000177 00000-0 93270-4 0 9990
2 00012 32.9003 289.7271 1666073 169.8734 194.0232 11.44390116305565
Epoch (UTC): | 26 January 2021 17:38:29 |
Eccentricity: | 0.1666073 |
inclination: | 32.9003° |
perigee height: | 554 km |
apogee height: | 3325 km |
right ascension of ascending node: | 289.7271° |
argument of perigee: | 169.8734° |
revolutions per day: | 11.44390116 |
mean anomaly at epoch: | 194.0232° |
orbit number at epoch: | 30556 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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