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 16611U 86018A 13142.16931349 .00003123 00000-0 19925-3 0 6888
2 16611 082.5044 062.8479 0015604 083.6863 276.6142 15.08268904484126
| Epoch (UTC): | 22 May 2013 04:03:48 |
| Eccentricity: | 0.0015604 |
| inclination: | 82.5044° |
| perigee height: | 530 km |
| apogee height: | 552 km |
| right ascension of ascending node: | 62.8479° |
| argument of perigee: | 83.6863° |
| revolutions per day: | 15.08268904 |
| mean anomaly at epoch: | 276.6142° |
| orbit number at epoch: | 48412 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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