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 23270.62002222 .00000298 00000-0 15063-3 0 9991
2 27665 39.5761 310.4722 0008418 56.8885 93.5924 14.28831435 78971
| Epoch (UTC): | 27 September 2023 14:52:49 |
| Eccentricity: | 0.0008418 |
| inclination: | 39.5761° |
| perigee height: | 789 km |
| apogee height: | 801 km |
| right ascension of ascending node: | 310.4722° |
| argument of perigee: | 56.8885° |
| revolutions per day: | 14.28831435 |
| mean anomaly at epoch: | 93.5924° |
| orbit number at epoch: | 7897 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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