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 24837U 97030B 13170.31251008 .00000267 00000-0 88107-4 0 4038
2 24837 086.3964 239.8647 0002337 111.6564 291.2577 14.34217045837844
| Epoch (UTC): | 19 June 2013 07:30:00 |
| Eccentricity: | 0.0002337 |
| inclination: | 86.3964° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 239.8647° |
| argument of perigee: | 111.6564° |
| revolutions per day: | 14.34217045 |
| mean anomaly at epoch: | 291.2577° |
| orbit number at epoch: | 83784 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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