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 25469U 98051C 13143.43869184 .00000382 00000-0 12924-3 0 2508
2 25469 086.3962 282.9699 0002266 107.0048 309.7881 14.34217631769889
| Epoch (UTC): | 23 May 2013 10:31:42 |
| Eccentricity: | 0.0002266 |
| inclination: | 86.3962° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 282.9699° |
| argument of perigee: | 107.0048° |
| revolutions per day: | 14.34217631 |
| mean anomaly at epoch: | 309.7881° |
| orbit number at epoch: | 76988 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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