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 13343.84858392 .00000571 00000-0 13679-3 0 7532
2 25994 098.2093 056.2221 0001117 105.0836 255.0473 14.57116819743499
| Epoch (UTC): | 09 December 2013 20:21:57 |
| Eccentricity: | 0.0001117 |
| inclination: | 98.2093° |
| perigee height: | 702 km |
| apogee height: | 703 km |
| right ascension of ascending node: | 56.2221° |
| argument of perigee: | 105.0836° |
| revolutions per day: | 14.57116819 |
| mean anomaly at epoch: | 255.0473° |
| orbit number at epoch: | 74349 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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