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 09903U 77024A 13168.79482359 .00000150 00000-0 79790-4 0 5344
2 09903 081.2527 057.4541 0038637 089.4724 335.4781 14.08062929859559
| Epoch (UTC): | 17 June 2013 19:04:32 |
| Eccentricity: | 0.0038637 |
| inclination: | 81.2527° |
| perigee height: | 838 km |
| apogee height: | 894 km |
| right ascension of ascending node: | 57.4541° |
| argument of perigee: | 89.4724° |
| revolutions per day: | 14.08062929 |
| mean anomaly at epoch: | 335.4781° |
| orbit number at epoch: | 85955 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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