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 53386U 22096S 23349.50812669 .12323112 26664-5 12188-2 0 9998
2 53386 97.3697 265.0468 0003974 138.3952 221.7649 16.38312123 76085
| Epoch (UTC): | 15 December 2023 12:11:42 |
| Eccentricity: | 0.0003974 |
| inclination: | 97.3697° |
| perigee height: | 168 km |
| apogee height: | 173 km |
| right ascension of ascending node: | 265.0468° |
| argument of perigee: | 138.3952° |
| revolutions per day: | 16.38312123 |
| mean anomaly at epoch: | 221.7649° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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