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 14443U 77121BF 24357.63564244 .00007466 00000-0 15323-2 0 9998
2 14443 65.5796 72.7989 0094161 90.0295 271.1598 14.58442402257061
Epoch (UTC): | 22 December 2024 15:15:19 |
Eccentricity: | 0.0094161 |
inclination: | 65.5796° |
perigee height: | 631 km |
apogee height: | 765 km |
right ascension of ascending node: | 72.7989° |
argument of perigee: | 90.0295° |
revolutions per day: | 14.58442402 |
mean anomaly at epoch: | 271.1598° |
orbit number at epoch: | 25706 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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