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 17295U 87003A 18113.69772404 .00000639 00000-0 32640-4 0 9992
2 17295 82.5170 199.4303 0004821 122.5777 237.5921 15.14892334705960
| Epoch (UTC): | 23 April 2018 16:44:43 |
| Eccentricity: | 0.0004821 |
| inclination: | 82.5170° |
| perigee height: | 518 km |
| apogee height: | 524 km |
| right ascension of ascending node: | 199.4303° |
| argument of perigee: | 122.5777° |
| revolutions per day: | 15.14892334 |
| mean anomaly at epoch: | 237.5921° |
| orbit number at epoch: | 70596 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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