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 31222U 99025BLC 24279.01026200 .00035913 00000-0 28137-2 0 9994
2 31222 98.6690 300.8822 0203938 36.8310 324.6715 14.85902876935150
Epoch (UTC): | 05 October 2024 00:14:46 |
Eccentricity: | 0.0203938 |
inclination: | 98.6690° |
perigee height: | 468 km |
apogee height: | 753 km |
right ascension of ascending node: | 300.8822° |
argument of perigee: | 36.8310° |
revolutions per day: | 14.85902876 |
mean anomaly at epoch: | 324.6715° |
orbit number at epoch: | 93515 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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