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 39144U 13016C 13117.34335161 .19973685 12818-4 24541-3 0 9992
2 39144 051.6041 280.4425 0014016 040.2321 322.2775 16.48613285 786
| Epoch (UTC): | 27 April 2013 08:14:25 |
| Eccentricity: | 0.0014016 |
| inclination: | 51.6041° |
| perigee height: | 134 km |
| apogee height: | 152 km |
| right ascension of ascending node: | 280.4425° |
| argument of perigee: | 40.2321° |
| revolutions per day: | 16.48613285 |
| mean anomaly at epoch: | 322.2775° |
| orbit number at epoch: | 78 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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