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 25342U 98032A 13142.46855133 .00000158 00000-0 49279-4 0 3289
2 25342 086.3967 125.6236 0002275 108.9359 037.5348 14.34219982786007
| Epoch (UTC): | 22 May 2013 11:14:42 |
| Eccentricity: | 0.0002275 |
| inclination: | 86.3967° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 125.6236° |
| argument of perigee: | 108.9359° |
| revolutions per day: | 14.34219982 |
| mean anomaly at epoch: | 37.5348° |
| orbit number at epoch: | 78600 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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