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 00115U 60002D 24311.13520818 .00012629 00000-0 12391-2 0 9992
2 00115 48.1663 102.3444 0028435 139.7976 220.5050 14.92113696430114
Epoch (UTC): | 06 November 2024 03:14:41 |
Eccentricity: | 0.0028435 |
inclination: | 48.1663° |
perigee height: | 571 km |
apogee height: | 611 km |
right ascension of ascending node: | 102.3444° |
argument of perigee: | 139.7976° |
revolutions per day: | 14.92113696 |
mean anomaly at epoch: | 220.5050° |
orbit number at epoch: | 43011 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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