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 85U 61004C 24318.15993097 .00056067 00000-0 54051-2 0 9996
2 85 38.7181 271.1980 0204221 296.9874 61.0169 14.77646962162203
Epoch (UTC): | 13 November 2024 03:50:18 |
Eccentricity: | 0.0204221 |
inclination: | 38.7181° |
perigee height: | 493 km |
apogee height: | 780 km |
right ascension of ascending node: | 271.1980° |
argument of perigee: | 296.9874° |
revolutions per day: | 14.77646962 |
mean anomaly at epoch: | 61.0169° |
orbit number at epoch: | 16220 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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