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 23159.57190121 .00000930 00000-0 21464-3 0 9996
2 35933 98.5152 31.0610 0006794 53.0363 307.1456 14.57624747728035
Epoch (UTC): | 08 June 2023 13:43:32 |
Eccentricity: | 0.0006794 |
inclination: | 98.5152° |
perigee height: | 696 km |
apogee height: | 705 km |
right ascension of ascending node: | 31.0610° |
argument of perigee: | 53.0363° |
revolutions per day: | 14.57624747 |
mean anomaly at epoch: | 307.1456° |
orbit number at epoch: | 72803 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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