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 26907U 01040C 13096.79931447 0.00000020 00000-0 30830-4 0 05
2 26907 63.4213 340.2950 0230000 358.6374 1.3626 13.41164013 01
| Epoch (UTC): | 06 April 2013 19:11:00 |
| Eccentricity: | 0.0230000 |
| inclination: | 63.4213° |
| perigee height: | 933 km |
| apogee height: | 1277 km |
| right ascension of ascending node: | 340.2950° |
| argument of perigee: | 358.6374° |
| revolutions per day: | 13.41164013 |
| mean anomaly at epoch: | 1.3626° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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