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 20104U 89050B 21024.94736878 .00000061 00000-0 45141-4 0 9996
2 20104 82.9554 273.7538 0044920 93.7605 266.8690 13.77328374585781
| Epoch (UTC): | 24 January 2021 22:44:12 |
| Eccentricity: | 0.0044920 |
| inclination: | 82.9554° |
| perigee height: | 940 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 273.7538° |
| argument of perigee: | 93.7605° |
| revolutions per day: | 13.77328374 |
| mean anomaly at epoch: | 266.8690° |
| orbit number at epoch: | 58578 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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