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 15060.01174362 .00001225 00000-0 20494-3 0 9995
2 25510 031.4350 271.2161 0331037 202.5040 312.3887 14.36421085856523
| Epoch (UTC): | 01 March 2015 00:16:54 |
| Eccentricity: | 0.0331037 |
| inclination: | 31.4350° |
| perigee height: | 534 km |
| apogee height: | 1007 km |
| right ascension of ascending node: | 271.2161° |
| argument of perigee: | 202.5040° |
| revolutions per day: | 14.36421085 |
| mean anomaly at epoch: | 312.3887° |
| orbit number at epoch: | 85652 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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