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 18264.89825788 -.00000038 +00000-0 +44139-5 0 9999
2 27431 099.0868 244.8664 0014565 233.6669 126.3157 14.09659838841392
| Epoch (UTC): | 21 September 2018 21:33:29 |
| Eccentricity: | 0.0014565 |
| inclination: | 99.0868° |
| perigee height: | 850 km |
| apogee height: | 871 km |
| right ascension of ascending node: | 244.8664° |
| argument of perigee: | 233.6669° |
| revolutions per day: | 14.09659838 |
| mean anomaly at epoch: | 126.3157° |
| orbit number at epoch: | 84139 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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