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 is defined by the following mean orbital elements,
1 26631U 00079A 16189.05109989 .20884161 29118-5 17845-3 0 9994
2 26631 97.5215 309.5274 0021517 337.3677 22.8343 16.50691252866752
| Epoch (UTC): | 07 July 2016 01:13:35 |
| Eccentricity: | 0.0021517 |
| inclination: | 97.5215° |
| perigee height: | 123 km |
| apogee height: | 151 km |
| right ascension of ascending node: | 309.5274° |
| argument of perigee: | 337.3677° |
| revolutions per day: | 16.50691252 |
| mean anomaly at epoch: | 22.8343° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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