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 25199.27730659 .00000127 00000-0 74617-4 0 9993
2 09662 81.2763 131.8984 0053075 111.2253 249.4594 14.01252572479861
| Epoch (UTC): | 18 July 2025 06:39:19 |
| Eccentricity: | 0.0053075 |
| inclination: | 81.2763° |
| perigee height: | 851 km |
| apogee height: | 928 km |
| right ascension of ascending node: | 131.8984° |
| argument of perigee: | 111.2253° |
| revolutions per day: | 14.01252572 |
| mean anomaly at epoch: | 249.4594° |
| orbit number at epoch: | 47986 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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