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 is defined by the following mean orbital elements,
1 53383U 22096P 24130.81992993 .14758822 26758-5 27755-3 0 9990
2 53383 97.3659 53.1715 0009376 214.1978 145.8722 16.46939767 98590
| Epoch (UTC): | 09 May 2024 19:40:41 |
| Eccentricity: | 0.0009376 |
| inclination: | 97.3659° |
| perigee height: | 141 km |
| apogee height: | 153 km |
| right ascension of ascending node: | 53.1715° |
| argument of perigee: | 214.1978° |
| revolutions per day: | 16.46939767 |
| mean anomaly at epoch: | 145.8722° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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