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 26905U 01040A 13105.04653678 0.00000000 00000-0 00000-0 0 09
2 26905 63.4260 320.6159 0234000 357.8015 2.1985 13.40661466 01
| Epoch (UTC): | 15 April 2013 01:07:00 |
| Eccentricity: | 0.0234000 |
| inclination: | 63.4260° |
| perigee height: | 931 km |
| apogee height: | 1282 km |
| right ascension of ascending node: | 320.6159° |
| argument of perigee: | 357.8015° |
| revolutions per day: | 13.40661466 |
| mean anomaly at epoch: | 2.1985° |
| 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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