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 00047U 60007C 23030.47474693 .00000447 00000-0 12219-3 0 9999
2 00047 66.6657 115.4752 0231241 321.5631 36.9189 14.42579360272680
| Epoch (UTC): | 30 January 2023 11:23:38 |
| Eccentricity: | 0.0231241 |
| inclination: | 66.6657° |
| perigee height: | 585 km |
| apogee height: | 915 km |
| right ascension of ascending node: | 115.4752° |
| argument of perigee: | 321.5631° |
| revolutions per day: | 14.42579360 |
| mean anomaly at epoch: | 36.9189° |
| orbit number at epoch: | 27268 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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