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 14552U 83122B 14114.85297867 .00000646 00000-0 76891-4 0 8345
2 14552 082.5257 072.2150 0016783 353.0050 066.0689 14.82800482638825
| Epoch (UTC): | 24 April 2014 20:28:17 |
| Eccentricity: | 0.0016783 |
| inclination: | 82.5257° |
| perigee height: | 609 km |
| apogee height: | 632 km |
| right ascension of ascending node: | 72.2150° |
| argument of perigee: | 353.0050° |
| revolutions per day: | 14.82800482 |
| mean anomaly at epoch: | 66.0689° |
| orbit number at epoch: | 63882 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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