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 13138.77477288 .00001295 00000-0 14920-3 0 7750
2 22626 082.5235 004.4406 0020426 023.9448 336.2713 14.84833062 84722
| Epoch (UTC): | 18 May 2013 18:35:40 |
| Eccentricity: | 0.0020426 |
| inclination: | 82.5235° |
| perigee height: | 600 km |
| apogee height: | 628 km |
| right ascension of ascending node: | 4.4406° |
| argument of perigee: | 23.9448° |
| revolutions per day: | 14.84833062 |
| mean anomaly at epoch: | 336.2713° |
| orbit number at epoch: | 8472 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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