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 27432U 02024C 24310.58727330 .00000320 00000-0 18847-3 0 9997
2 27432 98.9579 353.4806 0049755 331.5515 145.8140 14.14401166160096
Epoch (UTC): | 05 November 2024 14:05:40 |
Eccentricity: | 0.0049755 |
inclination: | 98.9579° |
perigee height: | 808 km |
apogee height: | 880 km |
right ascension of ascending node: | 353.4806° |
argument of perigee: | 331.5515° |
revolutions per day: | 14.14401166 |
mean anomaly at epoch: | 145.8140° |
orbit number at epoch: | 16009 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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