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 24257.54002861 .00000343 00000-0 32067-3 0 9998
2 116 66.8120 20.6674 0075045 357.7978 2.2759 13.92096741207887
| Epoch (UTC): | 13 September 2024 12:57:38 |
| Eccentricity: | 0.0075045 |
| inclination: | 66.8120° |
| perigee height: | 866 km |
| apogee height: | 976 km |
| right ascension of ascending node: | 20.6674° |
| argument of perigee: | 357.7978° |
| revolutions per day: | 13.92096741 |
| mean anomaly at epoch: | 2.2759° |
| orbit number at epoch: | 20788 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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