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 00116U 61015A 23331.48469361 .00000121 00000-0 15077-3 0 9991
2 00116 66.8109 12.4792 0079035 211.4209 148.2137 13.91971929166873
| Epoch (UTC): | 27 November 2023 11:37:57 |
| Eccentricity: | 0.0079035 |
| inclination: | 66.8109° |
| perigee height: | 864 km |
| apogee height: | 979 km |
| right ascension of ascending node: | 12.4792° |
| argument of perigee: | 211.4209° |
| revolutions per day: | 13.91971929 |
| mean anomaly at epoch: | 148.2137° |
| orbit number at epoch: | 16687 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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