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 19339.25528991 .00001806 00000-0 40859-3 0 9994
2 85 38.7713 296.2499 0388620 278.8587 76.8357 14.20018208903315
| Epoch (UTC): | 05 December 2019 06:07:37 |
| Eccentricity: | 0.0388620 |
| inclination: | 38.7713° |
| perigee height: | 545 km |
| apogee height: | 1105 km |
| right ascension of ascending node: | 296.2499° |
| argument of perigee: | 278.8587° |
| revolutions per day: | 14.20018208 |
| mean anomaly at epoch: | 76.8357° |
| orbit number at epoch: | 90331 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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