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 53375U 22096F 24139.46500842 .14922257 26026-5 18572-3 0 9999
2 53375 97.3662 61.3006 0013463 227.7775 132.2387 16.48987082 99881
| Epoch (UTC): | 18 May 2024 11:09:36 |
| Eccentricity: | 0.0013463 |
| inclination: | 97.3662° |
| perigee height: | 133 km |
| apogee height: | 151 km |
| right ascension of ascending node: | 61.3006° |
| argument of perigee: | 227.7775° |
| revolutions per day: | 16.48987082 |
| mean anomaly at epoch: | 132.2387° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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