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 23332.10744182 .00000349 00000-0 17014-3 0 9996
2 27665 39.5770 357.1796 0008242 99.7182 294.9757 14.28877780 87773
| Epoch (UTC): | 28 November 2023 02:34:42 |
| Eccentricity: | 0.0008242 |
| inclination: | 39.5770° |
| perigee height: | 789 km |
| apogee height: | 801 km |
| right ascension of ascending node: | 357.1796° |
| argument of perigee: | 99.7182° |
| revolutions per day: | 14.28877780 |
| mean anomaly at epoch: | 294.9757° |
| orbit number at epoch: | 8777 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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