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 25510U 98061C 15027.55499061 .00001635 00000-0 27858-3 0 563
2 25510 031.4369 097.1172 0331366 274.9894 240.8321 14.36299251851852
| Epoch (UTC): | 27 January 2015 13:19:11 |
| Eccentricity: | 0.0331366 |
| inclination: | 31.4369° |
| perigee height: | 534 km |
| apogee height: | 1007 km |
| right ascension of ascending node: | 97.1172° |
| argument of perigee: | 274.9894° |
| revolutions per day: | 14.36299251 |
| mean anomaly at epoch: | 240.8321° |
| orbit number at epoch: | 85185 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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