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 23336.87997002 .00066972 00000-0 99254-3 0 9994
2 40910 97.4484 354.4472 0004423 210.9556 149.1438 15.55021781455056
| Epoch (UTC): | 02 December 2023 21:07:09 |
| Eccentricity: | 0.0004423 |
| inclination: | 97.4484° |
| perigee height: | 399 km |
| apogee height: | 405 km |
| right ascension of ascending node: | 354.4472° |
| argument of perigee: | 210.9556° |
| revolutions per day: | 15.55021781 |
| mean anomaly at epoch: | 149.1438° |
| orbit number at epoch: | 45505 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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