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 27431U 02024B 23161.10354327 .00000086 00000-0 74996-4 0 9996
2 27431 99.0984 191.3429 0016535 98.8306 261.4737 14.09862745 84100
| Epoch (UTC): | 10 June 2023 02:29:06 |
| Eccentricity: | 0.0016535 |
| inclination: | 99.0984° |
| perigee height: | 848 km |
| apogee height: | 872 km |
| right ascension of ascending node: | 191.3429° |
| argument of perigee: | 98.8306° |
| revolutions per day: | 14.09862745 |
| mean anomaly at epoch: | 261.4737° |
| orbit number at epoch: | 8410 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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