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 23533U 95015A 24337.84926257 .00000602 00000-0 32291-3 0 9996
2 23533 98.8193 345.9138 0006181 326.2803 86.4167 14.16739487533709
Epoch (UTC): | 02 December 2024 20:22:56 |
Eccentricity: | 0.0006181 |
inclination: | 98.8193° |
perigee height: | 832 km |
apogee height: | 841 km |
right ascension of ascending node: | 345.9138° |
argument of perigee: | 326.2803° |
revolutions per day: | 14.16739487 |
mean anomaly at epoch: | 86.4167° |
orbit number at epoch: | 53370 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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