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 53381U 22096M 24157.64770976 .10376759 26036-5 35585-3 0 9993
2 53381 97.3632 80.6996 0010424 217.1606 142.8975 16.43656695102745
| Epoch (UTC): | 05 June 2024 15:32:42 |
| Eccentricity: | 0.0010424 |
| inclination: | 97.3632° |
| perigee height: | 149 km |
| apogee height: | 163 km |
| right ascension of ascending node: | 80.6996° |
| argument of perigee: | 217.1606° |
| revolutions per day: | 16.43656695 |
| mean anomaly at epoch: | 142.8975° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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