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 26901U 01039B 13140.52400240 .00009050 00000-0 25562-2 0 7441
2 26901 007.0109 160.9269 7036550 307.1217 296.4077 02.58908114103341
| Epoch (UTC): | 20 May 2013 12:34:33 |
| Eccentricity: | 0.7036550 |
| inclination: | 7.0109° |
| perigee height: | 261 km |
| apogee height: | 31788 km |
| right ascension of ascending node: | 160.9269° |
| argument of perigee: | 307.1217° |
| revolutions per day: | 2.58908114 |
| mean anomaly at epoch: | 296.4077° |
| orbit number at epoch: | 10334 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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