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 26088.11356472 +.00000000 +00000-0 +26704-4 0 00004
2 17160 82.9306 204.9064 0038387 208.2542 325.5726 13.74913013 04
| Epoch (UTC): | 29 March 2026 02:43:31 |
| Eccentricity: | 0.0038387 |
| inclination: | 82.9306° |
| perigee height: | 954 km |
| apogee height: | 1010 km |
| right ascension of ascending node: | 204.9064° |
| argument of perigee: | 208.2542° |
| revolutions per day: | 13.74913013 |
| mean anomaly at epoch: | 325.5726° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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