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 23151.09703415 .00000116 00000-0 91623-4 0 9999
2 27431 99.0991 181.2254 0016374 125.2722 234.9982 14.09859932 82693
| Epoch (UTC): | 31 May 2023 02:19:43 |
| Eccentricity: | 0.0016374 |
| inclination: | 99.0991° |
| perigee height: | 848 km |
| apogee height: | 872 km |
| right ascension of ascending node: | 181.2254° |
| argument of perigee: | 125.2722° |
| revolutions per day: | 14.09859932 |
| mean anomaly at epoch: | 234.9982° |
| orbit number at epoch: | 8269 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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