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 14552U 83122B 22139.41804181 .00000512 00000-0 59035-4 0 9991
2 14552 82.5258 193.8705 0017027 357.9566 2.1576 14.83672668 75633
| Epoch (UTC): | 19 May 2022 10:01:58 |
| Eccentricity: | 0.0017027 |
| inclination: | 82.5258° |
| perigee height: | 606 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 193.8705° |
| argument of perigee: | 357.9566° |
| revolutions per day: | 14.83672668 |
| mean anomaly at epoch: | 2.1576° |
| orbit number at epoch: | 7563 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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