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 13164.35246835 0.00000000 00000-0 00000-0 0 03
2 26907 63.4213 168.0284 0242000 358.5313 1.4686 13.41168907 05
| Epoch (UTC): | 13 June 2013 08:27:33 |
| Eccentricity: | 0.0242000 |
| inclination: | 63.4213° |
| perigee height: | 924 km |
| apogee height: | 1286 km |
| right ascension of ascending node: | 168.0284° |
| argument of perigee: | 358.5313° |
| revolutions per day: | 13.41168907 |
| mean anomaly at epoch: | 1.4686° |
| 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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