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 23335.01356239 .00087237 00000-0 13099-2 0 9999
2 40910 97.4481 352.5053 0004187 218.7953 141.3001 15.54584581454635
| Epoch (UTC): | 01 December 2023 00:19:31 |
| Eccentricity: | 0.0004187 |
| inclination: | 97.4481° |
| perigee height: | 400 km |
| apogee height: | 406 km |
| right ascension of ascending node: | 352.5053° |
| argument of perigee: | 218.7953° |
| revolutions per day: | 15.54584581 |
| mean anomaly at epoch: | 141.3001° |
| orbit number at epoch: | 45463 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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