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 27453U 02032A 23331.92089899 .00000415 00000-0 19469-3 0 9996
2 27453 98.7371 277.9445 0011787 170.7469 189.3930 14.25426045114130
| Epoch (UTC): | 27 November 2023 22:06:05 |
| Eccentricity: | 0.0011787 |
| inclination: | 98.7371° |
| perigee height: | 798 km |
| apogee height: | 815 km |
| right ascension of ascending node: | 277.9445° |
| argument of perigee: | 170.7469° |
| revolutions per day: | 14.25426045 |
| mean anomaly at epoch: | 189.3930° |
| orbit number at epoch: | 11413 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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