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 22227.66709879 .00000136 00000-0 12151-3 0 9999
2 20104 82.9550 212.3159 0042366 304.7051 55.0118 13.77361249663932
| Epoch (UTC): | 15 August 2022 16:00:37 |
| Eccentricity: | 0.0042366 |
| inclination: | 82.9550° |
| perigee height: | 942 km |
| apogee height: | 1004 km |
| right ascension of ascending node: | 212.3159° |
| argument of perigee: | 304.7051° |
| revolutions per day: | 13.77361249 |
| mean anomaly at epoch: | 55.0118° |
| orbit number at epoch: | 66393 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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