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 25994U 99068A 15059.17054921 .00001015 00000-0 23518-3 0 9999
2 25994 098.2162 135.1991 0001306 088.5370 271.5986 14.57136896808340
| Epoch (UTC): | 28 February 2015 04:05:35 |
| Eccentricity: | 0.0001306 |
| inclination: | 98.2162° |
| perigee height: | 701 km |
| apogee height: | 703 km |
| right ascension of ascending node: | 135.1991° |
| argument of perigee: | 88.5370° |
| revolutions per day: | 14.57136896 |
| mean anomaly at epoch: | 271.5986° |
| orbit number at epoch: | 80834 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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