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 43199U 18015H 23211.44374164 .08896774 26210-5 78857-3 0 9996
2 43199 97.5276 16.1198 0014611 280.6100 135.9568 16.38852523306706
| Epoch (UTC): | 30 July 2023 10:38:59 |
| Eccentricity: | 0.0014611 |
| inclination: | 97.5276° |
| perigee height: | 159 km |
| apogee height: | 178 km |
| right ascension of ascending node: | 16.1198° |
| argument of perigee: | 280.6100° |
| revolutions per day: | 16.38852523 |
| mean anomaly at epoch: | 135.9568° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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