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 39090U 13009E 19341.85959581 +.00000047 +00000-0 +31643-4 0 9994
2 39090 098.4697 184.7941 0009909 132.6545 227.5477 14.35108722355069
| Epoch (UTC): | 07 December 2019 20:37:49 |
| Eccentricity: | 0.0009909 |
| inclination: | 98.4697° |
| perigee height: | 767 km |
| apogee height: | 782 km |
| right ascension of ascending node: | 184.7941° |
| argument of perigee: | 132.6545° |
| revolutions per day: | 14.35108722 |
| mean anomaly at epoch: | 227.5477° |
| orbit number at epoch: | 35506 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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