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 23342.79850106 .00054242 00000-0 78135-3 0 9997
2 40910 97.4477 0.6122 0005204 184.4909 175.6300 15.55847245455845
| Epoch (UTC): | 08 December 2023 19:09:50 |
| Eccentricity: | 0.0005204 |
| inclination: | 97.4477° |
| perigee height: | 396 km |
| apogee height: | 403 km |
| right ascension of ascending node: | 0.6122° |
| argument of perigee: | 184.4909° |
| revolutions per day: | 15.55847245 |
| mean anomaly at epoch: | 175.6300° |
| orbit number at epoch: | 45584 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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