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 22626U 93024A 13169.03192371 .00000556 00000-0 62466-4 0 8007
2 22626 082.5232 336.0382 0018664 278.6767 081.2334 14.84883579 89213
| Epoch (UTC): | 18 June 2013 00:45:58 |
| Eccentricity: | 0.0018664 |
| inclination: | 82.5232° |
| perigee height: | 601 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 336.0382° |
| argument of perigee: | 278.6767° |
| revolutions per day: | 14.84883579 |
| mean anomaly at epoch: | 81.2334° |
| orbit number at epoch: | 8921 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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