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 14114.87627926 0.00077000 00000-0 35722-3 0 01
2 24680 97.5219 171.8383 0316790 232.7654 127.2344 15.36210555 07
| Epoch (UTC): | 24 April 2014 21:01:50 |
| Eccentricity: | 0.0316790 |
| inclination: | 97.5219° |
| perigee height: | 241 km |
| apogee height: | 674 km |
| right ascension of ascending node: | 171.8383° |
| argument of perigee: | 232.7654° |
| revolutions per day: | 15.36210555 |
| mean anomaly at epoch: | 127.2344° |
| 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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