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 25166.69760558 .00000339 00000-0 97816-4 0 9990
2 00047 66.6657 311.1866 0214650 45.6793 316.1686 14.44725995397850
| Epoch (UTC): | 15 June 2025 16:44:33 |
| Eccentricity: | 0.0214650 |
| inclination: | 66.6657° |
| perigee height: | 590 km |
| apogee height: | 896 km |
| right ascension of ascending node: | 311.1866° |
| argument of perigee: | 45.6793° |
| revolutions per day: | 14.44725995 |
| mean anomaly at epoch: | 316.1686° |
| orbit number at epoch: | 39785 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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