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 14113.42053564 .00000663 00000-0 22953-3 0 7816
2 25276 086.3996 048.0424 0002425 093.3896 266.7577 14.34210250841126
| Epoch (UTC): | 23 April 2014 10:05:34 |
| Eccentricity: | 0.0002425 |
| inclination: | 86.3996° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 48.0424° |
| argument of perigee: | 93.3896° |
| revolutions per day: | 14.34210250 |
| mean anomaly at epoch: | 266.7577° |
| orbit number at epoch: | 84112 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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