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 15495U 85009B 13139.52087681 .00000403 00000-0 46683-4 0 4634
2 15495 082.5233 142.0602 0020366 197.5454 309.0124 14.82893138529121
| Epoch (UTC): | 19 May 2013 12:30:03 |
| Eccentricity: | 0.0020366 |
| inclination: | 82.5233° |
| perigee height: | 606 km |
| apogee height: | 634 km |
| right ascension of ascending node: | 142.0602° |
| argument of perigee: | 197.5454° |
| revolutions per day: | 14.82893138 |
| mean anomaly at epoch: | 309.0124° |
| orbit number at epoch: | 52912 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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