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 24313.96901934 .00112529 00000-0 10875-1 0 9990
2 85 38.7182 294.5894 0206012 266.7581 90.9596 14.77055106161586
Epoch (UTC): | 08 November 2024 23:15:23 |
Eccentricity: | 0.0206012 |
inclination: | 38.7182° |
perigee height: | 494 km |
apogee height: | 783 km |
right ascension of ascending node: | 294.5894° |
argument of perigee: | 266.7581° |
revolutions per day: | 14.77055106 |
mean anomaly at epoch: | 90.9596° |
orbit number at epoch: | 16158 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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