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 13345.89529437 .00001118 00000-0 18835-3 0 7504
2 25510 031.4374 292.5851 0335823 233.0204 160.3260 14.35106162792653
| Epoch (UTC): | 11 December 2013 21:29:13 |
| Eccentricity: | 0.0335823 |
| inclination: | 31.4374° |
| perigee height: | 534 km |
| apogee height: | 1015 km |
| right ascension of ascending node: | 292.5851° |
| argument of perigee: | 233.0204° |
| revolutions per day: | 14.35106162 |
| mean anomaly at epoch: | 160.3260° |
| orbit number at epoch: | 79265 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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