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 26387U 00033D 13137.20423707 .00000597 00000-0 11563-3 0 2030
2 26387 098.1542 203.1232 0027440 027.1412 036.3418 14.66709900689037
| Epoch (UTC): | 17 May 2013 04:54:06 |
| Eccentricity: | 0.0027440 |
| inclination: | 98.1542° |
| perigee height: | 652 km |
| apogee height: | 691 km |
| right ascension of ascending node: | 203.1232° |
| argument of perigee: | 27.1412° |
| revolutions per day: | 14.66709900 |
| mean anomaly at epoch: | 36.3418° |
| orbit number at epoch: | 68903 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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