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 43801U 18099AV 25043.64122001 .06767571 24241-5 19069-2 0 9997
2 43801 97.3348 119.0287 0009390 287.1501 72.8764 16.27654057340212
| Epoch (UTC): | 12 February 2025 15:23:21 |
| Eccentricity: | 0.0009390 |
| inclination: | 97.3348° |
| perigee height: | 192 km |
| apogee height: | 205 km |
| right ascension of ascending node: | 119.0287° |
| argument of perigee: | 287.1501° |
| revolutions per day: | 16.27654057 |
| mean anomaly at epoch: | 72.8764° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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