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 24280.81738860 .00000344 00000-0 32118-3 0 9997
2 00116 66.8108 323.7351 0077044 341.6369 18.1932 13.92110042210625
| Epoch (UTC): | 06 October 2024 19:37:02 |
| Eccentricity: | 0.0077044 |
| inclination: | 66.8108° |
| perigee height: | 865 km |
| apogee height: | 977 km |
| right ascension of ascending node: | 323.7351° |
| argument of perigee: | 341.6369° |
| revolutions per day: | 13.92110042 |
| mean anomaly at epoch: | 18.1932° |
| orbit number at epoch: | 21062 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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