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 25510U 98061C 14070.49916172 .00002151 00000-0 37489-3 0 8170
2 25510 031.4360 140.2522 0334323 305.1862 175.1523 14.35484805805538
| Epoch (UTC): | 11 March 2014 11:58:47 |
| Eccentricity: | 0.0334323 |
| inclination: | 31.4360° |
| perigee height: | 534 km |
| apogee height: | 1012 km |
| right ascension of ascending node: | 140.2522° |
| argument of perigee: | 305.1862° |
| revolutions per day: | 14.35484805 |
| mean anomaly at epoch: | 175.1523° |
| orbit number at epoch: | 80553 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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