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 25064U 97074B 13145.47985120 .00009070 00000-0 24206-3 0 9021
2 25064 034.9688 259.6444 0005175 036.6739 034.4089 15.37323375861285
| Epoch (UTC): | 25 May 2013 11:30:59 |
| Eccentricity: | 0.0005175 |
| inclination: | 34.9688° |
| perigee height: | 450 km |
| apogee height: | 457 km |
| right ascension of ascending node: | 259.6444° |
| argument of perigee: | 36.6739° |
| revolutions per day: | 15.37323375 |
| mean anomaly at epoch: | 34.4089° |
| orbit number at epoch: | 86128 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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