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 54684U 22167C 25064.68183564 .08547514 26414-5 93170-3 0 9992
2 54684 97.5856 230.7463 0011725 277.2083 82.7881 16.37185507124845
| Epoch (UTC): | 05 March 2025 16:21:50 |
| Eccentricity: | 0.0011725 |
| inclination: | 97.5856° |
| perigee height: | 165 km |
| apogee height: | 181 km |
| right ascension of ascending node: | 230.7463° |
| argument of perigee: | 277.2083° |
| revolutions per day: | 16.37185507 |
| mean anomaly at epoch: | 82.7881° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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