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 24287.01686000 .00000872 00000-0 37316-3 0 9998
2 27665 39.5741 166.8080 0007805 10.6534 123.3140 14.29160391133417
| Epoch (UTC): | 13 October 2024 00:24:16 |
| Eccentricity: | 0.0007805 |
| inclination: | 39.5741° |
| perigee height: | 789 km |
| apogee height: | 800 km |
| right ascension of ascending node: | 166.8080° |
| argument of perigee: | 10.6534° |
| revolutions per day: | 14.29160391 |
| mean anomaly at epoch: | 123.3140° |
| orbit number at epoch: | 13341 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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