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 16273.83419471 0.00000500 00000-0 17774-3 0 02
2 31702 63.3712 261.3273 0247315 0.7957 359.2043 14.18514618 06
| Epoch (UTC): | 29 September 2016 20:01:14 |
| Eccentricity: | 0.0247315 |
| inclination: | 63.3712° |
| perigee height: | 652 km |
| apogee height: | 1008 km |
| right ascension of ascending node: | 261.3273° |
| argument of perigee: | 0.7957° |
| revolutions per day: | 14.18514618 |
| mean anomaly at epoch: | 359.2043° |
| 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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