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 43866U 18106A 25282.10864139 0.00000000 00000-0 00000-0 0 07
2 43866 98.6175 220.4900 0003489 154.8441 205.1558 14.26736736 04
| Epoch (UTC): | 09 October 2025 02:36:26 |
| Eccentricity: | 0.0003489 |
| inclination: | 98.6175° |
| perigee height: | 800 km |
| apogee height: | 805 km |
| right ascension of ascending node: | 220.4900° |
| argument of perigee: | 154.8441° |
| revolutions per day: | 14.26736736 |
| mean anomaly at epoch: | 205.1558° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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