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 15392U 84115B 14110.48146366 .00000317 00000-0 14910-3 0 1579
2 15392 021.4919 182.6233 1035081 315.8480 149.3607 12.45411453340063
| Epoch (UTC): | 20 April 2014 11:33:18 |
| Eccentricity: | 0.1035081 |
| inclination: | 21.4919° |
| perigee height: | 670 km |
| apogee height: | 2297 km |
| right ascension of ascending node: | 182.6233° |
| argument of perigee: | 315.8480° |
| revolutions per day: | 12.45411453 |
| mean anomaly at epoch: | 149.3607° |
| orbit number at epoch: | 34006 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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