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 00085U 61004C 24305.44412031 .00159368 00000-0 15937-1 0 9995
2 00085 38.7174 342.0693 0213625 205.6758 153.3269 14.74610523160362
Epoch (UTC): | 31 October 2024 10:39:31 |
Eccentricity: | 0.0213625 |
inclination: | 38.7174° |
perigee height: | 496 km |
apogee height: | 796 km |
right ascension of ascending node: | 342.0693° |
argument of perigee: | 205.6758° |
revolutions per day: | 14.74610523 |
mean anomaly at epoch: | 153.3269° |
orbit number at epoch: | 16036 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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