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 24282.19956682 .00002038 00000-0 82757-3 0 9993
2 27665 39.5749 191.3653 0008404 339.3801 178.4559 14.29157989132859
| Epoch (UTC): | 08 October 2024 04:47:22 |
| Eccentricity: | 0.0008404 |
| inclination: | 39.5749° |
| perigee height: | 788 km |
| apogee height: | 800 km |
| right ascension of ascending node: | 191.3653° |
| argument of perigee: | 339.3801° |
| revolutions per day: | 14.29157989 |
| mean anomaly at epoch: | 178.4559° |
| orbit number at epoch: | 13285 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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