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 37224U 10062C 13142.40880882 0.00001755 00000-0 00000-0 0 07
2 37224 71.9717 281.1793 0017576 47.2060 313.0586 14.78573364 02
| Epoch (UTC): | 22 May 2013 09:48:41 |
| Eccentricity: | 0.0017576 |
| inclination: | 71.9717° |
| perigee height: | 621 km |
| apogee height: | 646 km |
| right ascension of ascending node: | 281.1793° |
| argument of perigee: | 47.2060° |
| revolutions per day: | 14.78573364 |
| mean anomaly at epoch: | 313.0586° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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