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 23151.59381198 .00000148 00000-0 11000-3 0 9999
2 27431 99.0991 181.7277 0016394 123.9550 236.3180 14.09860153 82681
| Epoch (UTC): | 31 May 2023 14:15:05 |
| Eccentricity: | 0.0016394 |
| inclination: | 99.0991° |
| perigee height: | 848 km |
| apogee height: | 872 km |
| right ascension of ascending node: | 181.7277° |
| argument of perigee: | 123.9550° |
| revolutions per day: | 14.09860153 |
| mean anomaly at epoch: | 236.3180° |
| orbit number at epoch: | 8268 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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