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 42016U 17008BW 19345.67839632 +.00001232 +00000-0 +50816-4 0 9997
2 42016 097.3850 050.7950 0004563 267.7836 092.2880 15.25930063156735
| Epoch (UTC): | 11 December 2019 16:16:53 |
| Eccentricity: | 0.0004563 |
| inclination: | 97.3850° |
| perigee height: | 485 km |
| apogee height: | 491 km |
| right ascension of ascending node: | 50.7950° |
| argument of perigee: | 267.7836° |
| revolutions per day: | 15.25930063 |
| mean anomaly at epoch: | 92.2880° |
| orbit number at epoch: | 15673 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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