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 00117U 61015B 25340.85629484 .00000021 00000-0 77006-4 0 9999
2 00117 66.8115 114.0181 0071185 70.8286 290.0479 13.90164004267326
| Epoch (UTC): | 06 December 2025 20:33:03 |
| Eccentricity: | 0.0071185 |
| inclination: | 66.8115° |
| perigee height: | 876 km |
| apogee height: | 980 km |
| right ascension of ascending node: | 114.0181° |
| argument of perigee: | 70.8286° |
| revolutions per day: | 13.90164004 |
| mean anomaly at epoch: | 290.0479° |
| orbit number at epoch: | 26732 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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