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 18221.89118090 0.00008800 00000-0 86277-4 0 03
2 39232 97.9065 283.9371 0525834 79.8767 280.1232 14.79038931 04
| Epoch (UTC): | 09 August 2018 21:23:18 |
| Eccentricity: | 0.0525834 |
| inclination: | 97.9065° |
| perigee height: | 264 km |
| apogee height: | 1001 km |
| right ascension of ascending node: | 283.9371° |
| argument of perigee: | 79.8767° |
| revolutions per day: | 14.79038931 |
| mean anomaly at epoch: | 280.1232° |
| 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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