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 19325.28513162 -.00000082 00000-0 -38320-5 0 9992
2 116 66.8095 359.5389 0073489 160.4224 199.9704 13.91761647963200
| Epoch (UTC): | 21 November 2019 06:50:35 |
| Eccentricity: | 0.0073489 |
| inclination: | 66.8095° |
| perigee height: | 869 km |
| apogee height: | 976 km |
| right ascension of ascending node: | 359.5389° |
| argument of perigee: | 160.4224° |
| revolutions per day: | 13.91761647 |
| mean anomaly at epoch: | 199.9704° |
| orbit number at epoch: | 96320 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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