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 22147.50955179 .00000515 00000-0 21776-3 0 9997
2 00020 33.3391 175.3827 1664314 69.0304 307.9971 11.56207872312669
| Epoch (UTC): | 27 May 2022 12:13:45 |
| Eccentricity: | 0.1664314 |
| inclination: | 33.3391° |
| perigee height: | 508 km |
| apogee height: | 3258 km |
| right ascension of ascending node: | 175.3827° |
| argument of perigee: | 69.0304° |
| revolutions per day: | 11.56207872 |
| mean anomaly at epoch: | 307.9971° |
| orbit number at epoch: | 31266 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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