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 31702U 07027B 14196.85139225 0.00000400 00000-0 17392-3 0 07
2 31702 63.3790 89.9319 0149000 348.7074 11.2926 14.18148329 01
| Epoch (UTC): | 15 July 2014 20:26:00 |
| Eccentricity: | 0.0149000 |
| inclination: | 63.3790° |
| perigee height: | 724 km |
| apogee height: | 939 km |
| right ascension of ascending node: | 89.9319° |
| argument of perigee: | 348.7074° |
| revolutions per day: | 14.18148329 |
| mean anomaly at epoch: | 11.2926° |
| 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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