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 24278.89401163 .00001202 00000-0 50206-3 0 9990
2 27665 39.5749 208.2160 0008754 319.2236 90.2115 14.29145236132252
| Epoch (UTC): | 04 October 2024 21:27:22 |
| Eccentricity: | 0.0008754 |
| inclination: | 39.5749° |
| perigee height: | 788 km |
| apogee height: | 801 km |
| right ascension of ascending node: | 208.2160° |
| argument of perigee: | 319.2236° |
| revolutions per day: | 14.29145236 |
| mean anomaly at epoch: | 90.2115° |
| orbit number at epoch: | 13225 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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