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 23156.70352130 .00000034 00000-0 44996-4 0 9996
2 27431 99.0987 186.8943 0016510 110.3774 249.9171 14.09861441 83402
| Epoch (UTC): | 05 June 2023 16:53:04 |
| Eccentricity: | 0.0016510 |
| inclination: | 99.0987° |
| perigee height: | 848 km |
| apogee height: | 872 km |
| right ascension of ascending node: | 186.8943° |
| argument of perigee: | 110.3774° |
| revolutions per day: | 14.09861441 |
| mean anomaly at epoch: | 249.9171° |
| orbit number at epoch: | 8340 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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