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 23318U 26017.84221377 +.00000000 +00000-0 +41108-4 0 00008
2 23318 82.5424 137.5949 0023762 42.5347 317.7702 14.80842381 03
| Epoch (UTC): | 17 January 2026 20:12:47 |
| Eccentricity: | 0.0023762 |
| inclination: | 82.5424° |
| perigee height: | 610 km |
| apogee height: | 643 km |
| right ascension of ascending node: | 137.5949° |
| argument of perigee: | 42.5347° |
| revolutions per day: | 14.80842381 |
| mean anomaly at epoch: | 317.7702° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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