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 24255.52839525 .00000340 00000-0 31827-3 0 9999
2 116 66.8118 25.5873 0074880 359.2196 0.8754 13.92094977207602
| Epoch (UTC): | 11 September 2024 12:40:53 |
| Eccentricity: | 0.0074880 |
| inclination: | 66.8118° |
| perigee height: | 866 km |
| apogee height: | 976 km |
| right ascension of ascending node: | 25.5873° |
| argument of perigee: | 359.2196° |
| revolutions per day: | 13.92094977 |
| mean anomaly at epoch: | 0.8754° |
| orbit number at epoch: | 20760 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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