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 23148.46748365 .00000216 00000-0 84466-4 0 9999
2 27386 98.2295 119.2815 0001282 89.0847 20.4098 14.38348563113125
| Epoch (UTC): | 28 May 2023 11:13:10 |
| Eccentricity: | 0.0001282 |
| inclination: | 98.2295° |
| perigee height: | 763 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 119.2815° |
| argument of perigee: | 89.0847° |
| revolutions per day: | 14.38348563 |
| mean anomaly at epoch: | 20.4098° |
| orbit number at epoch: | 11312 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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