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 470U 61015FG 24357.95470833 .00001667 00000-0 10000-2 0 9997
2 470 66.2291 226.6819 0074062 290.9577 68.3592 14.08163030236629
| Epoch (UTC): | 22 December 2024 22:54:46 |
| Eccentricity: | 0.0074062 |
| inclination: | 66.2291° |
| perigee height: | 812 km |
| apogee height: | 919 km |
| right ascension of ascending node: | 226.6819° |
| argument of perigee: | 290.9577° |
| revolutions per day: | 14.08163030 |
| mean anomaly at epoch: | 68.3592° |
| orbit number at epoch: | 23662 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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