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 23336.58183529 .00002274 00000-0 50412-3 0 9996
2 35933 98.4872 211.9010 0004792 211.3341 148.7572 14.58120537753829
Epoch (UTC): | 02 December 2023 13:57:50 |
Eccentricity: | 0.0004792 |
inclination: | 98.4872° |
perigee height: | 696 km |
apogee height: | 702 km |
right ascension of ascending node: | 211.9010° |
argument of perigee: | 211.3341° |
revolutions per day: | 14.58120537 |
mean anomaly at epoch: | 148.7572° |
orbit number at epoch: | 75382 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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