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 09662U 77002B 25189.35207963 .00000039 00000-0 17414-4 0 9992
2 09662 81.2756 141.3834 0052768 138.4876 222.0317 14.01251480478476
| Epoch (UTC): | 08 July 2025 08:26:59 |
| Eccentricity: | 0.0052768 |
| inclination: | 81.2756° |
| perigee height: | 851 km |
| apogee height: | 928 km |
| right ascension of ascending node: | 141.3834° |
| argument of perigee: | 138.4876° |
| revolutions per day: | 14.01251480 |
| mean anomaly at epoch: | 222.0317° |
| orbit number at epoch: | 47847 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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