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 25396U 98043C 18350.05842358 .00000017 00000-0 25932-4 0 9994
2 25396 98.6462 288.5348 0002859 153.2001 206.9327 14.24500631 62032
| Epoch (UTC): | 16 December 2018 01:24:07 |
| Eccentricity: | 0.0002859 |
| inclination: | 98.6462° |
| perigee height: | 808 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 288.5348° |
| argument of perigee: | 153.2001° |
| revolutions per day: | 14.24500631 |
| mean anomaly at epoch: | 206.9327° |
| orbit number at epoch: | 6203 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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