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 23092.14949054 .00039905 00000-0 12422-2 0 9994
2 40910 97.4691 104.2834 0012110 48.4466 17.3101 15.33109005417227
| Epoch (UTC): | 02 April 2023 03:35:15 |
| Eccentricity: | 0.0012110 |
| inclination: | 97.4691° |
| perigee height: | 458 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 104.2834° |
| argument of perigee: | 48.4466° |
| revolutions per day: | 15.33109005 |
| mean anomaly at epoch: | 17.3101° |
| orbit number at epoch: | 41722 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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