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 00020U 59007A 22146.81838054 .00000539 00000-0 22774-3 0 9997
2 00020 33.3391 177.8475 1664300 65.3602 311.1014 11.56207172312589
| Epoch (UTC): | 26 May 2022 19:38:28 |
| Eccentricity: | 0.1664300 |
| inclination: | 33.3391° |
| perigee height: | 508 km |
| apogee height: | 3258 km |
| right ascension of ascending node: | 177.8475° |
| argument of perigee: | 65.3602° |
| revolutions per day: | 11.56207172 |
| mean anomaly at epoch: | 311.1014° |
| orbit number at epoch: | 31258 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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