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 26931U 01043C 23344.67960052 .00000184 00000-0 10122-3 0 9992
2 26931 67.0509 101.0608 0005652 259.5088 100.5377 14.31064803158996
Epoch (UTC): | 10 December 2023 16:18:37 |
Eccentricity: | 0.0005652 |
inclination: | 67.0509° |
perigee height: | 784 km |
apogee height: | 792 km |
right ascension of ascending node: | 101.0608° |
argument of perigee: | 259.5088° |
revolutions per day: | 14.31064803 |
mean anomaly at epoch: | 100.5377° |
orbit number at epoch: | 15899 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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