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 14104.99949453 .00000622 00000-0 98156-4 0 8429
2 25510 031.4367 302.8914 0334082 250.3469 272.4294 14.35604664810496
| Epoch (UTC): | 14 April 2014 23:59:16 |
| Eccentricity: | 0.0334082 |
| inclination: | 31.4367° |
| perigee height: | 534 km |
| apogee height: | 1012 km |
| right ascension of ascending node: | 302.8914° |
| argument of perigee: | 250.3469° |
| revolutions per day: | 14.35604664 |
| mean anomaly at epoch: | 272.4294° |
| orbit number at epoch: | 81049 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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