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 25407U 98045B 13338.89944725 .00000028 00000-0 38843-4 0 3433
2 25407 071.0122 232.6687 0007984 355.7159 076.6176 14.15628507793573
| Epoch (UTC): | 04 December 2013 21:35:12 |
| Eccentricity: | 0.0007984 |
| inclination: | 71.0122° |
| perigee height: | 834 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 232.6687° |
| argument of perigee: | 355.7159° |
| revolutions per day: | 14.15628507 |
| mean anomaly at epoch: | 76.6176° |
| orbit number at epoch: | 79357 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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