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 20580U 90037B 22021.18838866 .00001468 00000-0 77279-4 0 9994
2 20580 28.4710 64.1073 0002362 245.6684 164.4825 15.09958017544196
| Epoch (UTC): | 21 January 2022 04:31:16 |
| Eccentricity: | 0.0002362 |
| inclination: | 28.4710° |
| perigee height: | 535 km |
| apogee height: | 538 km |
| right ascension of ascending node: | 64.1073° |
| argument of perigee: | 245.6684° |
| revolutions per day: | 15.09958017 |
| mean anomaly at epoch: | 164.4825° |
| orbit number at epoch: | 54419 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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