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 23467U 95003A 13103.82477963 0.00000000 00000-0 00000-0 0 06
2 23467 7.7567 39.3173 0003714 266.3847 93.5849 1.00261433 01
| Epoch (UTC): | 13 April 2013 19:47:40 |
| Eccentricity: | 0.0003714 |
| inclination: | 7.7567° |
| perigee height: | 35773 km |
| apogee height: | 35805 km |
| right ascension of ascending node: | 39.3173° |
| argument of perigee: | 266.3847° |
| revolutions per day: | 1.00261433 |
| mean anomaly at epoch: | 93.5849° |
| 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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