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 22225.18858388 .00001761 00000-0 92741-4 0 9998
2 20580 28.4691 152.8122 0002387 287.0186 216.0583 15.10751138574801
| Epoch (UTC): | 13 August 2022 04:31:33 |
| Eccentricity: | 0.0002387 |
| inclination: | 28.4691° |
| perigee height: | 532 km |
| apogee height: | 535 km |
| right ascension of ascending node: | 152.8122° |
| argument of perigee: | 287.0186° |
| revolutions per day: | 15.10751138 |
| mean anomaly at epoch: | 216.0583° |
| orbit number at epoch: | 57480 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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