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 16270.48095831 .00001137 00000-0 60975-4 0 9999
2 17295 82.5148 44.3385 0002832 348.1020 12.0144 15.13993778619050
| Epoch (UTC): | 26 September 2016 11:32:34 |
| Eccentricity: | 0.0002832 |
| inclination: | 82.5148° |
| perigee height: | 522 km |
| apogee height: | 526 km |
| right ascension of ascending node: | 44.3385° |
| argument of perigee: | 348.1020° |
| revolutions per day: | 15.13993778 |
| mean anomaly at epoch: | 12.0144° |
| orbit number at epoch: | 61905 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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