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 19345.16325942 .00001659 00000-0 37924-3 0 9997
2 85 38.7700 266.1453 0387889 318.1298 39.0377 14.20037849904158
Epoch (UTC): | 11 December 2019 03:55:05 |
Eccentricity: | 0.0387889 |
inclination: | 38.7700° |
perigee height: | 546 km |
apogee height: | 1104 km |
right ascension of ascending node: | 266.1453° |
argument of perigee: | 318.1298° |
revolutions per day: | 14.20037849 |
mean anomaly at epoch: | 39.0377° |
orbit number at epoch: | 90415 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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