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 23342U 26018.55573185 +.00000000 +00000-0 +89368-4 0 00001
2 23342 97.6745 42.6311 0001263 115.6993 244.4353 14.84828420 03
| Epoch (UTC): | 18 January 2026 13:20:15 |
| Eccentricity: | 0.0001263 |
| inclination: | 97.6745° |
| perigee height: | 613 km |
| apogee height: | 615 km |
| right ascension of ascending node: | 42.6311° |
| argument of perigee: | 115.6993° |
| revolutions per day: | 14.84828420 |
| mean anomaly at epoch: | 244.4353° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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