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 23038.86360736 .00001017 00000-0 24569-3 0 9997
2 00047 66.6650 93.0247 0231822 315.5455 42.7245 14.42593915273899
| Epoch (UTC): | 07 February 2023 20:43:35 |
| Eccentricity: | 0.0231822 |
| inclination: | 66.6650° |
| perigee height: | 585 km |
| apogee height: | 915 km |
| right ascension of ascending node: | 93.0247° |
| argument of perigee: | 315.5455° |
| revolutions per day: | 14.42593915 |
| mean anomaly at epoch: | 42.7245° |
| orbit number at epoch: | 27389 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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