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 15494U 85009A 13168.38431288 .00001541 00000-0 88629-4 0 3106
2 15494 082.4853 261.2177 0004414 104.0100 300.3561 15.11768063547158
| Epoch (UTC): | 17 June 2013 09:13:24 |
| Eccentricity: | 0.0004414 |
| inclination: | 82.4853° |
| perigee height: | 528 km |
| apogee height: | 534 km |
| right ascension of ascending node: | 261.2177° |
| argument of perigee: | 104.0100° |
| revolutions per day: | 15.11768063 |
| mean anomaly at epoch: | 300.3561° |
| orbit number at epoch: | 54715 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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