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 15495U 85009B 17175.52731015 +.00000056 +00000-0 +39188-5 0 9996
2 15495 082.5233 180.5981 0018886 308.9639 050.9892 14.83770519729961
| Epoch (UTC): | 24 June 2017 12:39:19 |
| Eccentricity: | 0.0018886 |
| inclination: | 82.5233° |
| perigee height: | 604 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 180.5981° |
| argument of perigee: | 308.9639° |
| revolutions per day: | 14.83770519 |
| mean anomaly at epoch: | 50.9892° |
| orbit number at epoch: | 72996 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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