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 116U 61015A 19229.20603297 -.00000076 00000-0 57692-6 0 9992
2 116 66.8077 234.4105 0080974 226.3991 133.0350 13.91756749949822
| Epoch (UTC): | 17 August 2019 04:56:41 |
| Eccentricity: | 0.0080974 |
| inclination: | 66.8077° |
| perigee height: | 863 km |
| apogee height: | 981 km |
| right ascension of ascending node: | 234.4105° |
| argument of perigee: | 226.3991° |
| revolutions per day: | 13.91756749 |
| mean anomaly at epoch: | 133.0350° |
| orbit number at epoch: | 94982 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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