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 24254.73810982 .00000351 00000-0 32678-3 0 9994
2 00116 66.8117 27.5202 0074811 359.7747 0.3286 13.92094433206993
| Epoch (UTC): | 10 September 2024 17:42:52 |
| Eccentricity: | 0.0074811 |
| inclination: | 66.8117° |
| perigee height: | 866 km |
| apogee height: | 976 km |
| right ascension of ascending node: | 27.5202° |
| argument of perigee: | 359.7747° |
| revolutions per day: | 13.92094433 |
| mean anomaly at epoch: | 0.3286° |
| orbit number at epoch: | 20699 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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