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 31329U 99025BQH 24284.65502960 .00025692 00000-0 56705-2 0 9995
2 31329 98.8606 232.5845 0065835 323.7422 35.9321 14.55934704918470
Epoch (UTC): | 10 October 2024 15:43:14 |
Eccentricity: | 0.0065835 |
inclination: | 98.8606° |
perigee height: | 659 km |
apogee height: | 753 km |
right ascension of ascending node: | 232.5845° |
argument of perigee: | 323.7422° |
revolutions per day: | 14.55934704 |
mean anomaly at epoch: | 35.9321° |
orbit number at epoch: | 91847 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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