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 35933U 09051C 23335.62112953 .00002431 00000-0 53829-3 0 9993
2 35933 98.4872 210.9205 0004745 214.9406 145.1481 14.58115985753688
Epoch (UTC): | 01 December 2023 14:54:25 |
Eccentricity: | 0.0004745 |
inclination: | 98.4872° |
perigee height: | 696 km |
apogee height: | 702 km |
right ascension of ascending node: | 210.9205° |
argument of perigee: | 214.9406° |
revolutions per day: | 14.58115985 |
mean anomaly at epoch: | 145.1481° |
orbit number at epoch: | 75368 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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