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 25276U 98019E 14213.46863366 .00000173 00000-0 54671-4 0 9046
2 25276 086.3974 006.2138 0002191 108.8885 251.2549 14.34216803855460
| Epoch (UTC): | 01 August 2014 11:14:49 |
| Eccentricity: | 0.0002191 |
| inclination: | 86.3974° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 6.2138° |
| argument of perigee: | 108.8885° |
| revolutions per day: | 14.34216803 |
| mean anomaly at epoch: | 251.2549° |
| orbit number at epoch: | 85546 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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