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 10674U 78018A 18347.60385597 -.00000050 00000-0 16539-5 0 9993
2 10674 69.3628 20.9490 0165457 206.2279 285.5123 13.43609852 2519
| Epoch (UTC): | 13 December 2018 14:29:33 |
| Eccentricity: | 0.0165457 |
| inclination: | 69.3628° |
| perigee height: | 972 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 20.9490° |
| argument of perigee: | 206.2279° |
| revolutions per day: | 13.43609852 |
| mean anomaly at epoch: | 285.5123° |
| orbit number at epoch: | 251 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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