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 40071U 14037C 24262.80011829 .00004449 00000-0 51928-3 0 9991
2 40071 98.3277 179.5559 0007936 166.9543 193.1877 14.85699446551531
Epoch (UTC): | 18 September 2024 19:12:10 |
Eccentricity: | 0.0007936 |
inclination: | 98.3277° |
perigee height: | 606 km |
apogee height: | 617 km |
right ascension of ascending node: | 179.5559° |
argument of perigee: | 166.9543° |
revolutions per day: | 14.85699446 |
mean anomaly at epoch: | 193.1877° |
orbit number at epoch: | 55153 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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