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 20U 59007A 22144.13996908 .00000699 00000-0 29233-3 0 9997
2 20 33.3391 187.3990 1664243 51.1381 322.6333 11.56204175312301
| Epoch (UTC): | 24 May 2022 03:21:33 |
| Eccentricity: | 0.1664243 |
| inclination: | 33.3391° |
| perigee height: | 508 km |
| apogee height: | 3258 km |
| right ascension of ascending node: | 187.3990° |
| argument of perigee: | 51.1381° |
| revolutions per day: | 11.56204175 |
| mean anomaly at epoch: | 322.6333° |
| orbit number at epoch: | 31230 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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