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 33740U 99025DJD 24353.28243369 .00000466 00000-0 27800-3 0 9992
2 33740 98.7069 10.8713 0002413 94.5992 265.5456 14.12035771850733
Epoch (UTC): | 18 December 2024 06:46:42 |
Eccentricity: | 0.0002413 |
inclination: | 98.7069° |
perigee height: | 850 km |
apogee height: | 854 km |
right ascension of ascending node: | 10.8713° |
argument of perigee: | 94.5992° |
revolutions per day: | 14.12035771 |
mean anomaly at epoch: | 265.5456° |
orbit number at epoch: | 85073 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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