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 19322.48252953 -.00000081 00000-0 -31153-5 0 9995
2 116 66.8112 6.3893 0073628 162.4338 197.9314 13.91761764962811
| Epoch (UTC): | 18 November 2019 11:34:50 |
| Eccentricity: | 0.0073628 |
| inclination: | 66.8112° |
| perigee height: | 869 km |
| apogee height: | 976 km |
| right ascension of ascending node: | 6.3893° |
| argument of perigee: | 162.4338° |
| revolutions per day: | 13.91761764 |
| mean anomaly at epoch: | 197.9314° |
| orbit number at epoch: | 96281 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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