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 24262.71279187 .00000173 00000-0 19106-3 0 9990
2 116 66.8121 8.0156 0075463 354.2072 5.8126 13.92099519208608
| Epoch (UTC): | 18 September 2024 17:06:25 |
| Eccentricity: | 0.0075463 |
| inclination: | 66.8121° |
| perigee height: | 866 km |
| apogee height: | 976 km |
| right ascension of ascending node: | 8.0156° |
| argument of perigee: | 354.2072° |
| revolutions per day: | 13.92099519 |
| mean anomaly at epoch: | 5.8126° |
| orbit number at epoch: | 20860 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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