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 14068.87432413 .00000707 00000-0 16689-3 0 293
2 25994 098.2192 144.9477 0001472 099.8301 260.3042 14.57137291756603
| Epoch (UTC): | 09 March 2014 20:59:01 |
| Eccentricity: | 0.0001472 |
| inclination: | 98.2192° |
| perigee height: | 701 km |
| apogee height: | 703 km |
| right ascension of ascending node: | 144.9477° |
| argument of perigee: | 99.8301° |
| revolutions per day: | 14.57137291 |
| mean anomaly at epoch: | 260.3042° |
| orbit number at epoch: | 75660 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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