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 43666U 18083E 24066.92221879 .17137449 25508-5 30224-3 0 9998
2 43666 97.3150 111.6353 0013426 246.6021 113.3871 16.46850493298211
| Epoch (UTC): | 06 March 2024 22:07:59 |
| Eccentricity: | 0.0013426 |
| inclination: | 97.3150° |
| perigee height: | 139 km |
| apogee height: | 156 km |
| right ascension of ascending node: | 111.6353° |
| argument of perigee: | 246.6021° |
| revolutions per day: | 16.46850493 |
| mean anomaly at epoch: | 113.3871° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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