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 23335.78594009 .00110816 00000-0 16482-2 0 9991
2 40910 97.4484 353.3086 0004263 215.4173 144.6798 15.54757914454750
| Epoch (UTC): | 01 December 2023 18:51:45 |
| Eccentricity: | 0.0004263 |
| inclination: | 97.4484° |
| perigee height: | 400 km |
| apogee height: | 406 km |
| right ascension of ascending node: | 353.3086° |
| argument of perigee: | 215.4173° |
| revolutions per day: | 15.54757914 |
| mean anomaly at epoch: | 144.6798° |
| orbit number at epoch: | 45475 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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