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 24255.60023930 .00000347 00000-0 32371-3 0 9995
2 00116 66.8118 25.4116 0074884 359.1686 0.9257 13.92095078207116
| Epoch (UTC): | 11 September 2024 14:24:20 |
| Eccentricity: | 0.0074884 |
| inclination: | 66.8118° |
| perigee height: | 866 km |
| apogee height: | 976 km |
| right ascension of ascending node: | 25.4116° |
| argument of perigee: | 359.1686° |
| revolutions per day: | 13.92095078 |
| mean anomaly at epoch: | 0.9257° |
| orbit number at epoch: | 20711 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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