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 11681U 80007B 23267.22219118 .00000108 00000-0 96005-4 0 9991
2 11681 82.9335 153.9568 0037565 77.6817 41.3725 13.75550269191194
| Epoch (UTC): | 24 September 2023 05:19:57 |
| Eccentricity: | 0.0037565 |
| inclination: | 82.9335° |
| perigee height: | 952 km |
| apogee height: | 1007 km |
| right ascension of ascending node: | 153.9568° |
| argument of perigee: | 77.6817° |
| revolutions per day: | 13.75550269 |
| mean anomaly at epoch: | 41.3725° |
| orbit number at epoch: | 19119 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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