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 39444U 13066AE 23340.45296637 .00005806 00000-0 60913-3 0 9995
2 39444 97.6957 299.2187 0052993 64.5554 296.1133 14.88849775541257
| Epoch (UTC): | 06 December 2023 10:52:16 |
| Eccentricity: | 0.0052993 |
| inclination: | 97.6957° |
| perigee height: | 564 km |
| apogee height: | 638 km |
| right ascension of ascending node: | 299.2187° |
| argument of perigee: | 64.5554° |
| revolutions per day: | 14.88849775 |
| mean anomaly at epoch: | 296.1133° |
| orbit number at epoch: | 54125 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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