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 27665U 03005C 24276.93782306 .00001091 00000-0 45874-3 0 9995
2 27665 39.5749 218.1880 0008933 307.4663 104.8175 14.29140959131976
| Epoch (UTC): | 02 October 2024 22:30:27 |
| Eccentricity: | 0.0008933 |
| inclination: | 39.5749° |
| perigee height: | 788 km |
| apogee height: | 801 km |
| right ascension of ascending node: | 218.1880° |
| argument of perigee: | 307.4663° |
| revolutions per day: | 14.29140959 |
| mean anomaly at epoch: | 104.8175° |
| orbit number at epoch: | 13197 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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