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 22278.78654806 .00000418 00000-0 11880-3 0 9993
2 00047 66.6657 67.6826 0221067 47.1371 314.8066 14.42433219255851
| Epoch (UTC): | 05 October 2022 18:52:37 |
| Eccentricity: | 0.0221067 |
| inclination: | 66.6657° |
| perigee height: | 593 km |
| apogee height: | 908 km |
| right ascension of ascending node: | 67.6826° |
| argument of perigee: | 47.1371° |
| revolutions per day: | 14.42433219 |
| mean anomaly at epoch: | 314.8066° |
| orbit number at epoch: | 25585 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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