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 12744U 81053CM 23332.52044672 .00006246 00000-0 28922-2 0 9991
2 12744 82.9312 134.1580 0022049 68.2894 292.0631 14.20547566157265
Epoch (UTC): | 28 November 2023 12:29:26 |
Eccentricity: | 0.0022049 |
inclination: | 82.9312° |
perigee height: | 807 km |
apogee height: | 839 km |
right ascension of ascending node: | 134.1580° |
argument of perigee: | 68.2894° |
revolutions per day: | 14.20547566 |
mean anomaly at epoch: | 292.0631° |
orbit number at epoch: | 15726 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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