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 22024.50840557 .00001221 00000-0 62432-4 0 9995
2 20580 28.4712 42.1300 0002330 285.0338 208.0692 15.09965616544703
| Epoch (UTC): | 24 January 2022 12:12:06 |
| Eccentricity: | 0.0002330 |
| inclination: | 28.4712° |
| perigee height: | 535 km |
| apogee height: | 538 km |
| right ascension of ascending node: | 42.1300° |
| argument of perigee: | 285.0338° |
| revolutions per day: | 15.09965616 |
| mean anomaly at epoch: | 208.0692° |
| orbit number at epoch: | 54470 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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