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 14206.07316189 -.00000046 00000-0 -23524-4 0 8943
2 25276 086.3968 009.3056 0002162 115.9539 244.1880 14.34215642854401
| Epoch (UTC): | 25 July 2014 01:45:21 |
| Eccentricity: | 0.0002162 |
| inclination: | 86.3968° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 9.3056° |
| argument of perigee: | 115.9539° |
| revolutions per day: | 14.34215642 |
| mean anomaly at epoch: | 244.1880° |
| orbit number at epoch: | 85440 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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