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 27510U 02040C 13142.36362744 .00000034 00000-0 21667-3 0 8460
2 27510 005.2934 061.7243 7149370 282.0424 352.5940 02.27158845 89092
| Epoch (UTC): | 22 May 2013 08:43:37 |
| Eccentricity: | 0.7149370 |
| inclination: | 5.2934° |
| perigee height: | 590 km |
| apogee height: | 35542 km |
| right ascension of ascending node: | 61.7243° |
| argument of perigee: | 282.0424° |
| revolutions per day: | 2.27158845 |
| mean anomaly at epoch: | 352.5940° |
| orbit number at epoch: | 8909 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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