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 39152U 13018C 19341.53198014 .00000133 00000-0 24042-4 0 9995
2 39152 97.9106 67.9443 0016519 356.2857 3.8230 14.80754693357238
| Epoch (UTC): | 07 December 2019 12:46:03 |
| Eccentricity: | 0.0016519 |
| inclination: | 97.9106° |
| perigee height: | 615 km |
| apogee height: | 638 km |
| right ascension of ascending node: | 67.9443° |
| argument of perigee: | 356.2857° |
| revolutions per day: | 14.80754693 |
| mean anomaly at epoch: | 3.8230° |
| orbit number at epoch: | 35723 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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