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 117U 61015B 25189.19658147 -.00000042 00000-0 27031-4 0 9992
2 117 66.8122 123.7149 0077874 183.6864 176.3651 13.90138959246685
| Epoch (UTC): | 08 July 2025 04:43:04 |
| Eccentricity: | 0.0077874 |
| inclination: | 66.8122° |
| perigee height: | 871 km |
| apogee height: | 985 km |
| right ascension of ascending node: | 123.7149° |
| argument of perigee: | 183.6864° |
| revolutions per day: | 13.90138959 |
| mean anomaly at epoch: | 176.3651° |
| orbit number at epoch: | 24668 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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