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 16262U 85108A 13169.19379259 .00001125 00000-0 80881-4 0 1905
2 16262 082.4946 236.2475 0011892 260.3049 099.6834 15.03285902498922
| Epoch (UTC): | 18 June 2013 04:39:03 |
| Eccentricity: | 0.0011892 |
| inclination: | 82.4946° |
| perigee height: | 548 km |
| apogee height: | 565 km |
| right ascension of ascending node: | 236.2475° |
| argument of perigee: | 260.3049° |
| revolutions per day: | 15.03285902 |
| mean anomaly at epoch: | 99.6834° |
| orbit number at epoch: | 49892 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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