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 31701U 07027A 15023.20998592 0.00000000 00000-0 00000-0 0 06
2 31701 63.4030 155.8263 0121000 35.4476 324.5524 13.40670071 07
| Epoch (UTC): | 23 January 2015 05:02:22 |
| Eccentricity: | 0.0121000 |
| inclination: | 63.4030° |
| perigee height: | 1016 km |
| apogee height: | 1197 km |
| right ascension of ascending node: | 155.8263° |
| argument of perigee: | 35.4476° |
| revolutions per day: | 13.40670071 |
| mean anomaly at epoch: | 324.5524° |
| 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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