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 23336.04337663 .00106212 00000-0 15763-2 0 9998
2 40910 97.4484 353.5766 0004298 214.1201 145.9777 15.54834370454790
| Epoch (UTC): | 02 December 2023 01:02:27 |
| Eccentricity: | 0.0004298 |
| inclination: | 97.4484° |
| perigee height: | 400 km |
| apogee height: | 405 km |
| right ascension of ascending node: | 353.5766° |
| argument of perigee: | 214.1201° |
| revolutions per day: | 15.54834370 |
| mean anomaly at epoch: | 145.9777° |
| orbit number at epoch: | 45479 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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