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 19348.82066741 +.00001462 +00000-0 +33817-3 0 9991
2 85 038.7689 247.5068 0387362 342.4694 016.2996 14.20048892904698
| Epoch (UTC): | 14 December 2019 19:41:45 |
| Eccentricity: | 0.0387362 |
| inclination: | 38.7689° |
| perigee height: | 546 km |
| apogee height: | 1104 km |
| right ascension of ascending node: | 247.5068° |
| argument of perigee: | 342.4694° |
| revolutions per day: | 14.20048892 |
| mean anomaly at epoch: | 16.2996° |
| orbit number at epoch: | 90469 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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