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 23405U 94077B 17268.78798740 +.00000044 +00000-0 +47306-4 0 9997
2 23405 070.9845 003.8854 0003164 215.5660 144.5252 14.15203371179496
| Epoch (UTC): | 25 September 2017 18:54:42 |
| Eccentricity: | 0.0003164 |
| inclination: | 70.9845° |
| perigee height: | 839 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 3.8854° |
| argument of perigee: | 215.5660° |
| revolutions per day: | 14.15203371 |
| mean anomaly at epoch: | 144.5252° |
| orbit number at epoch: | 17949 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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