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 23334.66042005 .00002728 00000-0 60280-3 0 9994
2 35933 98.4875 209.9399 0004703 218.4093 141.6770 14.58112312753625
Epoch (UTC): | 30 November 2023 15:51:00 |
Eccentricity: | 0.0004703 |
inclination: | 98.4875° |
perigee height: | 696 km |
apogee height: | 702 km |
right ascension of ascending node: | 209.9399° |
argument of perigee: | 218.4093° |
revolutions per day: | 14.58112312 |
mean anomaly at epoch: | 141.6770° |
orbit number at epoch: | 75362 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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