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 15030.86756026 .00002045 00000-0 23247-3 0 5059
2 26546 064.5563 170.9446 0017537 325.8142 034.1837 14.88962750777280
| Epoch (UTC): | 30 January 2015 20:49:17 |
| Eccentricity: | 0.0017537 |
| inclination: | 64.5563° |
| perigee height: | 589 km |
| apogee height: | 613 km |
| right ascension of ascending node: | 170.9446° |
| argument of perigee: | 325.8142° |
| revolutions per day: | 14.88962750 |
| mean anomaly at epoch: | 34.1837° |
| orbit number at epoch: | 77728 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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