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 26017.34272308 +.00000000 +00000-0 +84090-4 0 00007
2 23342 97.6746 41.4630 0001216 115.1662 244.9679 14.84826698 02
| Epoch (UTC): | 17 January 2026 08:13:31 |
| Eccentricity: | 0.0001216 |
| inclination: | 97.6746° |
| perigee height: | 613 km |
| apogee height: | 615 km |
| right ascension of ascending node: | 41.4630° |
| argument of perigee: | 115.1662° |
| revolutions per day: | 14.84826698 |
| mean anomaly at epoch: | 244.9679° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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