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 52188U 22033AH 24064.08974563 .16469240 25228-5 29977-3 0 9995
2 52188 97.3006 159.6485 0014560 272.2143 87.7493 16.46530331107992
| Epoch (UTC): | 04 March 2024 02:09:14 |
| Eccentricity: | 0.0014560 |
| inclination: | 97.3006° |
| perigee height: | 139 km |
| apogee height: | 158 km |
| right ascension of ascending node: | 159.6485° |
| argument of perigee: | 272.2143° |
| revolutions per day: | 16.46530331 |
| mean anomaly at epoch: | 87.7493° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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