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 22226.24302747 .00001764 00000-0 92890-4 0 9997
2 20580 28.4693 145.8232 0002400 299.3853 189.8894 15.10754857574960
| Epoch (UTC): | 14 August 2022 05:49:57 |
| Eccentricity: | 0.0002400 |
| inclination: | 28.4693° |
| perigee height: | 532 km |
| apogee height: | 535 km |
| right ascension of ascending node: | 145.8232° |
| argument of perigee: | 299.3853° |
| revolutions per day: | 15.10754857 |
| mean anomaly at epoch: | 189.8894° |
| orbit number at epoch: | 57496 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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