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 25338.69797507 .00000023 00000-0 78791-4 0 9994
2 117 66.8113 119.2794 0071127 72.4862 288.3972 13.90163580267028
| Epoch (UTC): | 04 December 2025 16:45:05 |
| Eccentricity: | 0.0071127 |
| inclination: | 66.8113° |
| perigee height: | 876 km |
| apogee height: | 980 km |
| right ascension of ascending node: | 119.2794° |
| argument of perigee: | 72.4862° |
| revolutions per day: | 13.90163580 |
| mean anomaly at epoch: | 288.3972° |
| orbit number at epoch: | 26702 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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