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 24287.84822023 .00000664 00000-0 29215-3 0 9994
2 27665 39.5739 162.5698 0007705 16.4240 80.2878 14.29160845133535
| Epoch (UTC): | 13 October 2024 20:21:26 |
| Eccentricity: | 0.0007705 |
| inclination: | 39.5739° |
| perigee height: | 789 km |
| apogee height: | 800 km |
| right ascension of ascending node: | 162.5698° |
| argument of perigee: | 16.4240° |
| revolutions per day: | 14.29160845 |
| mean anomaly at epoch: | 80.2878° |
| orbit number at epoch: | 13353 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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