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 26481U 00050A 16070.83870556 .05360644 00000-0 11920-3 0 9996
2 26481 97.1411 83.0170 0005769 180.6035 179.6337 16.46415765870203
| Epoch (UTC): | 10 March 2016 20:07:44 |
| Eccentricity: | 0.0005769 |
| inclination: | 97.1411° |
| perigee height: | 145 km |
| apogee height: | 152 km |
| right ascension of ascending node: | 83.0170° |
| argument of perigee: | 180.6035° |
| revolutions per day: | 16.46415765 |
| mean anomaly at epoch: | 179.6337° |
| orbit number at epoch: | 87020 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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