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 21023.85639782 .00000141 00000-0 76236-4 0 9998
2 00012 32.9001 299.8023 1666016 154.7307 214.5109 11.44389263305232
Epoch (UTC): | 23 January 2021 20:33:12 |
Eccentricity: | 0.1666016 |
inclination: | 32.9001° |
perigee height: | 554 km |
apogee height: | 3325 km |
right ascension of ascending node: | 299.8023° |
argument of perigee: | 154.7307° |
revolutions per day: | 11.44389263 |
mean anomaly at epoch: | 214.5109° |
orbit number at epoch: | 30523 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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