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 40046U 14033AN 24279.43063279 .00027163 00000-0 29736-2 0 9991
2 40046 97.6745 87.5890 0046062 274.0340 85.5611 14.86967291554596
| Epoch (UTC): | 05 October 2024 10:20:06 |
| Eccentricity: | 0.0046062 |
| inclination: | 97.6745° |
| perigee height: | 575 km |
| apogee height: | 639 km |
| right ascension of ascending node: | 87.5890° |
| argument of perigee: | 274.0340° |
| revolutions per day: | 14.86967291 |
| mean anomaly at epoch: | 85.5611° |
| orbit number at epoch: | 55459 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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