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 24680U 96072A 13139.83691041 0.00011300 00000-0 19420-3 0 00
2 24680 97.5795 193.5125 0339063 330.8293 29.1706 15.06515021 03
| Epoch (UTC): | 19 May 2013 20:05:09 |
| Eccentricity: | 0.0339063 |
| inclination: | 97.5795° |
| perigee height: | 312 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 193.5125° |
| argument of perigee: | 330.8293° |
| revolutions per day: | 15.06515021 |
| mean anomaly at epoch: | 29.1706° |
| 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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