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 40907U 15049J 24276.83156877 .00246763 00000-0 18674-2 0 9991
2 40907 97.4593 301.4249 0003483 200.3305 159.7820 15.71663417501462
| Epoch (UTC): | 02 October 2024 19:57:27 |
| Eccentricity: | 0.0003483 |
| inclination: | 97.4593° |
| perigee height: | 352 km |
| apogee height: | 356 km |
| right ascension of ascending node: | 301.4249° |
| argument of perigee: | 200.3305° |
| revolutions per day: | 15.71663417 |
| mean anomaly at epoch: | 159.7820° |
| orbit number at epoch: | 50146 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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