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 27386U 02009A 23265.95148855 .00000285 00000-0 10709-3 0 9995
2 27386 98.2424 231.9916 0001176 86.3871 341.8999 14.38409649130012
| Epoch (UTC): | 22 September 2023 22:50:08 |
| Eccentricity: | 0.0001176 |
| inclination: | 98.2424° |
| perigee height: | 763 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 231.9916° |
| argument of perigee: | 86.3871° |
| revolutions per day: | 14.38409649 |
| mean anomaly at epoch: | 341.8999° |
| orbit number at epoch: | 13001 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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