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 00060U 60014A 12087.77141234 .11240700 12162-4 82585-3 0 10
2 00060 049.8769 297.0017 0014319 253.4265 106.9983 16.39420536586174
| Epoch (UTC): | 27 March 2012 18:30:50 |
| Eccentricity: | 0.0014319 |
| inclination: | 49.8769° |
| perigee height: | 158 km |
| apogee height: | 177 km |
| right ascension of ascending node: | 297.0017° |
| argument of perigee: | 253.4265° |
| revolutions per day: | 16.39420536 |
| mean anomaly at epoch: | 106.9983° |
| orbit number at epoch: | 58617 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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