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 39232U 13043A 19277.80894614 0.00010000 00000-0 10147-3 0 06
2 39232 97.8900 338.5985 0523209 151.4477 208.5521 14.78993073 09
| Epoch (UTC): | 04 October 2019 19:24:52 |
| Eccentricity: | 0.0523209 |
| inclination: | 97.8900° |
| perigee height: | 266 km |
| apogee height: | 999 km |
| right ascension of ascending node: | 338.5985° |
| argument of perigee: | 151.4477° |
| revolutions per day: | 14.78993073 |
| mean anomaly at epoch: | 208.5521° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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