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 43793U 18099AM 25221.21166546 .13619297 25930-5 68059-3 0 9999
2 43793 97.4554 304.9540 0017217 272.8328 87.1002 16.40904822367265
| Epoch (UTC): | 09 August 2025 05:04:47 |
| Eccentricity: | 0.0017217 |
| inclination: | 97.4554° |
| perigee height: | 152 km |
| apogee height: | 174 km |
| right ascension of ascending node: | 304.9540° |
| argument of perigee: | 272.8328° |
| revolutions per day: | 16.40904822 |
| mean anomaly at epoch: | 87.1002° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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