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 00011U 59001A 22175.41935704 .00000304 00000-0 16516-3 0 9996
2 00011 32.8637 167.8398 1466516 92.8583 284.0163 11.86141979362483
| Epoch (UTC): | 24 June 2022 10:03:52 |
| Eccentricity: | 0.1466516 |
| inclination: | 32.8637° |
| perigee height: | 552 km |
| apogee height: | 2934 km |
| right ascension of ascending node: | 167.8398° |
| argument of perigee: | 92.8583° |
| revolutions per day: | 11.86141979 |
| mean anomaly at epoch: | 284.0163° |
| orbit number at epoch: | 36248 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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