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 52160U 22033D 24094.73483658 .16762466 25370-5 22337-3 0 9997
2 52160 97.2953 188.9413 0010894 266.4206 93.5852 16.48822409112610
| Epoch (UTC): | 03 April 2024 17:38:09 |
| Eccentricity: | 0.0010894 |
| inclination: | 97.2953° |
| perigee height: | 135 km |
| apogee height: | 149 km |
| right ascension of ascending node: | 188.9413° |
| argument of perigee: | 266.4206° |
| revolutions per day: | 16.48822409 |
| mean anomaly at epoch: | 93.5852° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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