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 data is extracted from the following two-line orbital elements,
1 40910U 15049M 23342.02668704 .00056244 00000-0 81252-3 0 9992
2 40910 97.4479 359.8078 0005089 187.3488 172.7693 15.55761140455720
| Epoch (UTC): | 08 December 2023 00:38:25 |
| Eccentricity: | 0.0005089 |
| inclination: | 97.4479° |
| perigee height: | 396 km |
| apogee height: | 403 km |
| right ascension of ascending node: | 359.8078° |
| argument of perigee: | 187.3488° |
| revolutions per day: | 15.55761140 |
| mean anomaly at epoch: | 172.7693° |
| orbit number at epoch: | 45572 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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