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 35105U 99025DKH 24353.15450346 .00003434 00000-0 94357-3 0 9999
2 35105 98.9007 310.3030 0115583 46.4816 314.5908 14.43814362893018
Epoch (UTC): | 18 December 2024 03:42:29 |
Eccentricity: | 0.0115583 |
inclination: | 98.9007° |
perigee height: | 663 km |
apogee height: | 828 km |
right ascension of ascending node: | 310.3030° |
argument of perigee: | 46.4816° |
revolutions per day: | 14.43814362 |
mean anomaly at epoch: | 314.5908° |
orbit number at epoch: | 89301 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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