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 35685U 09041E 18344.81406254 .00000076 00000-0 16023-4 0 9990
2 35685 98.2869 343.8232 0060195 100.4746 260.3258 14.84149804506605
| Epoch (UTC): | 10 December 2018 19:32:15 |
| Eccentricity: | 0.0060195 |
| inclination: | 98.2869° |
| perigee height: | 574 km |
| apogee height: | 658 km |
| right ascension of ascending node: | 343.8232° |
| argument of perigee: | 100.4746° |
| revolutions per day: | 14.84149804 |
| mean anomaly at epoch: | 260.3258° |
| orbit number at epoch: | 50660 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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