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 116U 61015A 23345.13630765 -.00000014 00000-0 48325-4 0 9991
2 116 66.8102 339.0935 0077976 202.2653 157.5036 13.91975955169277
| Epoch (UTC): | 11 December 2023 03:16:16 |
| Eccentricity: | 0.0077976 |
| inclination: | 66.8102° |
| perigee height: | 865 km |
| apogee height: | 978 km |
| right ascension of ascending node: | 339.0935° |
| argument of perigee: | 202.2653° |
| revolutions per day: | 13.91975955 |
| mean anomaly at epoch: | 157.5036° |
| orbit number at epoch: | 16927 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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