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 13140.83327988 .00000565 00000-0 10986-3 0 2063
2 26387 098.1539 206.7317 0027195 015.7800 118.2016 14.66716741689560
| Epoch (UTC): | 20 May 2013 19:59:55 |
| Eccentricity: | 0.0027195 |
| inclination: | 98.1539° |
| perigee height: | 652 km |
| apogee height: | 691 km |
| right ascension of ascending node: | 206.7317° |
| argument of perigee: | 15.7800° |
| revolutions per day: | 14.66716741 |
| mean anomaly at epoch: | 118.2016° |
| orbit number at epoch: | 68956 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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