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 43690U 18088A 24202.07135098 .09091031 -14183-5 72401-3 0 9993
2 43690 84.9804 154.7556 0010058 197.5723 162.5236 16.40010442317466
| Epoch (UTC): | 20 July 2024 01:42:44 |
| Eccentricity: | 0.0010058 |
| inclination: | 84.9804° |
| perigee height: | 159 km |
| apogee height: | 172 km |
| right ascension of ascending node: | 154.7556° |
| argument of perigee: | 197.5723° |
| revolutions per day: | 16.40010442 |
| mean anomaly at epoch: | 162.5236° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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