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 40906U 15049H 25047.62605869 .06460715 25777-5 82494-3 0 9990
2 40906 97.4284 83.7622 0006300 238.5188 121.5494 16.35922890522636
| Epoch (UTC): | 16 February 2025 15:01:31 |
| Eccentricity: | 0.0006300 |
| inclination: | 97.4284° |
| perigee height: | 172 km |
| apogee height: | 181 km |
| right ascension of ascending node: | 83.7622° |
| argument of perigee: | 238.5188° |
| revolutions per day: | 16.35922890 |
| mean anomaly at epoch: | 121.5494° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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