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 24260.43802350 .00000621 00000-0 27535-3 0 9997
2 27665 39.5760 302.2972 0008660 210.5991 165.1013 14.29119058129616
| Epoch (UTC): | 16 September 2024 10:30:45 |
| Eccentricity: | 0.0008660 |
| inclination: | 39.5760° |
| perigee height: | 788 km |
| apogee height: | 801 km |
| right ascension of ascending node: | 302.2972° |
| argument of perigee: | 210.5991° |
| revolutions per day: | 14.29119058 |
| mean anomaly at epoch: | 165.1013° |
| orbit number at epoch: | 12961 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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