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 17264.86657928 +.00000688 +00000-0 +35574-4 0 9993
2 17295 082.5145 049.8835 0004372 137.6372 222.5199 15.14607658673361
| Epoch (UTC): | 21 September 2017 20:47:52 |
| Eccentricity: | 0.0004372 |
| inclination: | 82.5145° |
| perigee height: | 519 km |
| apogee height: | 525 km |
| right ascension of ascending node: | 49.8835° |
| argument of perigee: | 137.6372° |
| revolutions per day: | 15.14607658 |
| mean anomaly at epoch: | 222.5199° |
| orbit number at epoch: | 67336 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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