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 39439U 13066Z 23087.44635324 .00010385 00000-0 10989-2 0 9991
2 39439 97.6734 55.4331 0057736 182.3030 177.7930 14.88112869504216
| Epoch (UTC): | 28 March 2023 10:42:44 |
| Eccentricity: | 0.0057736 |
| inclination: | 97.6734° |
| perigee height: | 563 km |
| apogee height: | 644 km |
| right ascension of ascending node: | 55.4331° |
| argument of perigee: | 182.3030° |
| revolutions per day: | 14.88112869 |
| mean anomaly at epoch: | 177.7930° |
| orbit number at epoch: | 50421 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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