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 23150.67122454 .00000096 00000-0 80475-4 0 9990
2 27431 99.0992 180.7948 0016362 126.3722 233.8960 14.09859799 82636
| Epoch (UTC): | 30 May 2023 16:06:33 |
| Eccentricity: | 0.0016362 |
| inclination: | 99.0992° |
| perigee height: | 848 km |
| apogee height: | 871 km |
| right ascension of ascending node: | 180.7948° |
| argument of perigee: | 126.3722° |
| revolutions per day: | 14.09859799 |
| mean anomaly at epoch: | 233.8960° |
| orbit number at epoch: | 8263 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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