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 33410U 08053C 24284.55881229 .00013742 00000-0 71920-3 0 9996
2 33410 97.8694 321.5737 0103980 213.6533 145.8065 15.11312291871436
Epoch (UTC): | 10 October 2024 13:24:41 |
Eccentricity: | 0.0103980 |
inclination: | 97.8694° |
perigee height: | 460 km |
apogee height: | 604 km |
right ascension of ascending node: | 321.5737° |
argument of perigee: | 213.6533° |
revolutions per day: | 15.11312291 |
mean anomaly at epoch: | 145.8065° |
orbit number at epoch: | 87143 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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