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 23343.41189486 .00000007 00000-0 64370-4 0 9998
2 00116 66.8103 343.3107 0078123 203.4320 156.3192 13.91975760168538
| Epoch (UTC): | 09 December 2023 09:53:07 |
| Eccentricity: | 0.0078123 |
| inclination: | 66.8103° |
| perigee height: | 864 km |
| apogee height: | 979 km |
| right ascension of ascending node: | 343.3107° |
| argument of perigee: | 203.4320° |
| revolutions per day: | 13.91975760 |
| mean anomaly at epoch: | 156.3192° |
| orbit number at epoch: | 16853 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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