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 13242U 82051B 24284.54211835 .00001094 00000-0 37779-3 0 9997
2 13242 74.0416 128.4128 0023973 31.0933 329.1633 14.36852478216964
Epoch (UTC): | 10 October 2024 13:00:39 |
Eccentricity: | 0.0023973 |
inclination: | 74.0416° |
perigee height: | 752 km |
apogee height: | 786 km |
right ascension of ascending node: | 128.4128° |
argument of perigee: | 31.0933° |
revolutions per day: | 14.36852478 |
mean anomaly at epoch: | 329.1633° |
orbit number at epoch: | 21696 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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