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 20093.37233334 -.00000011 +00000-0 +50560-4 0 9996
2 116 066.8118 034.2015 0069800 059.2782 301.5149 13.91767735981236
| Epoch (UTC): | 02 April 2020 08:56:09 |
| Eccentricity: | 0.0069800 |
| inclination: | 66.8118° |
| perigee height: | 871 km |
| apogee height: | 973 km |
| right ascension of ascending node: | 34.2015° |
| argument of perigee: | 59.2782° |
| revolutions per day: | 13.91767735 |
| mean anomaly at epoch: | 301.5149° |
| orbit number at epoch: | 98123 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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