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 26546U 00057B 16270.86448234 .00000692 00000-0 69313-4 0 9993
2 26546 64.5551 79.3816 0046688 256.1778 103.4657 14.90324168867413
| Epoch (UTC): | 26 September 2016 20:44:51 |
| Eccentricity: | 0.0046688 |
| inclination: | 64.5551° |
| perigee height: | 564 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 79.3816° |
| argument of perigee: | 256.1778° |
| revolutions per day: | 14.90324168 |
| mean anomaly at epoch: | 103.4657° |
| orbit number at epoch: | 86741 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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