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 00058U 60013A 24312.92534911 .00000208 00000-0 19096-3 0 9997
2 00058 28.3266 234.4519 0164796 33.3562 327.7247 13.46393689154997
Epoch (UTC): | 07 November 2024 22:12:30 |
Eccentricity: | 0.0164796 |
inclination: | 28.3266° |
perigee height: | 962 km |
apogee height: | 1208 km |
right ascension of ascending node: | 234.4519° |
argument of perigee: | 33.3562° |
revolutions per day: | 13.46393689 |
mean anomaly at epoch: | 327.7247° |
orbit number at epoch: | 15499 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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