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 53373U 22096D 24063.41486467 .07516655 25945-5 88211-3 0 9993
2 53373 97.3635 344.5166 0006006 175.3577 184.7778 16.36718985 88183
| Epoch (UTC): | 03 March 2024 09:57:24 |
| Eccentricity: | 0.0006006 |
| inclination: | 97.3635° |
| perigee height: | 170 km |
| apogee height: | 178 km |
| right ascension of ascending node: | 344.5166° |
| argument of perigee: | 175.3577° |
| revolutions per day: | 16.36718985 |
| mean anomaly at epoch: | 184.7778° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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