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 18349.93003498 -.00000040 00000-0 33594-5 0 9990
2 27431 99.0981 330.7384 0015485 1.0328 359.0871 14.09666170853436
| Epoch (UTC): | 15 December 2018 22:19:15 |
| Eccentricity: | 0.0015485 |
| inclination: | 99.0981° |
| perigee height: | 849 km |
| apogee height: | 872 km |
| right ascension of ascending node: | 330.7384° |
| argument of perigee: | 1.0328° |
| revolutions per day: | 14.09666170 |
| mean anomaly at epoch: | 359.0871° |
| orbit number at epoch: | 85343 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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