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 24277.23638009 .00001100 00000-0 46197-3 0 9999
2 27665 39.5749 216.6662 0008912 309.2875 200.9824 14.29141236132147
| Epoch (UTC): | 03 October 2024 05:40:23 |
| Eccentricity: | 0.0008912 |
| inclination: | 39.5749° |
| perigee height: | 788 km |
| apogee height: | 801 km |
| right ascension of ascending node: | 216.6662° |
| argument of perigee: | 309.2875° |
| revolutions per day: | 14.29141236 |
| mean anomaly at epoch: | 200.9824° |
| orbit number at epoch: | 13214 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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