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 22334.32419414 .00000545 00000-0 14555-3 0 9993
2 00047 66.6657 279.1019 0225832 5.8630 354.5033 14.42493070263864
| Epoch (UTC): | 30 November 2022 07:46:50 |
| Eccentricity: | 0.0225832 |
| inclination: | 66.6657° |
| perigee height: | 589 km |
| apogee height: | 911 km |
| right ascension of ascending node: | 279.1019° |
| argument of perigee: | 5.8630° |
| revolutions per day: | 14.42493070 |
| mean anomaly at epoch: | 354.5033° |
| orbit number at epoch: | 26386 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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