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 is defined by the following mean orbital elements,
1 17160U 26017.15840528 +.00000000 +00000-0 +26225-4 0 00008
2 17160 82.9264 257.5768 0039866 49.0674 117.0204 13.74911986 04
| Epoch (UTC): | 17 January 2026 03:48:06 |
| Eccentricity: | 0.0039866 |
| inclination: | 82.9264° |
| perigee height: | 953 km |
| apogee height: | 1011 km |
| right ascension of ascending node: | 257.5768° |
| argument of perigee: | 49.0674° |
| revolutions per day: | 13.74911986 |
| mean anomaly at epoch: | 117.0204° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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