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 25407U 98045B 15063.86081913 .00000097 00000-0 73554-4 0 9999
2 25407 071.0138 356.7619 0006474 024.8782 335.2652 14.15697452857953
| Epoch (UTC): | 04 March 2015 20:39:34 |
| Eccentricity: | 0.0006474 |
| inclination: | 71.0138° |
| perigee height: | 835 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 356.7619° |
| argument of perigee: | 24.8782° |
| revolutions per day: | 14.15697452 |
| mean anomaly at epoch: | 335.2652° |
| orbit number at epoch: | 85795 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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