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 19040.83749270 0.00005000 00000-0 53897-4 0 08
2 39232 97.9186 105.3242 0533551 201.3098 158.6901 14.75691029 07
| Epoch (UTC): | 09 February 2019 20:05:59 |
| Eccentricity: | 0.0533551 |
| inclination: | 97.9186° |
| perigee height: | 268 km |
| apogee height: | 1017 km |
| right ascension of ascending node: | 105.3242° |
| argument of perigee: | 201.3098° |
| revolutions per day: | 14.75691029 |
| mean anomaly at epoch: | 158.6901° |
| 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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