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 22179.72047548 .00000220 00000-0 73733-4 0 9992
2 00020 33.3562 60.5180 1664927 240.0735 102.4303 11.56229565316399
| Epoch (UTC): | 28 June 2022 17:17:29 |
| Eccentricity: | 0.1664927 |
| inclination: | 33.3562° |
| perigee height: | 507 km |
| apogee height: | 3258 km |
| right ascension of ascending node: | 60.5180° |
| argument of perigee: | 240.0735° |
| revolutions per day: | 11.56229565 |
| mean anomaly at epoch: | 102.4303° |
| orbit number at epoch: | 31639 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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