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 23340.17861997 .00000052 00000-0 98581-4 0 9993
2 116 66.8105 351.2181 0078361 205.6258 154.0930 13.91975252168584
| Epoch (UTC): | 06 December 2023 04:17:12 |
| Eccentricity: | 0.0078361 |
| inclination: | 66.8105° |
| perigee height: | 864 km |
| apogee height: | 979 km |
| right ascension of ascending node: | 351.2181° |
| argument of perigee: | 205.6258° |
| revolutions per day: | 13.91975252 |
| mean anomaly at epoch: | 154.0930° |
| orbit number at epoch: | 16858 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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