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 23339.53255947 .00001373 00000-0 30855-3 0 9996
2 35933 98.4872 214.9124 0004959 200.8283 159.2714 14.58130823754253
Epoch (UTC): | 05 December 2023 12:46:53 |
Eccentricity: | 0.0004959 |
inclination: | 98.4872° |
perigee height: | 696 km |
apogee height: | 703 km |
right ascension of ascending node: | 214.9124° |
argument of perigee: | 200.8283° |
revolutions per day: | 14.58130823 |
mean anomaly at epoch: | 159.2714° |
orbit number at epoch: | 75425 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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