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 23343U 26129.82076551 +.00000000 +00000-0 +42459-4 0 00000
2 23343 97.7019 158.1359 0007300 33.8127 139.4567 14.79469201 04
| Epoch (UTC): | 09 May 2026 19:41:54 |
| Eccentricity: | 0.0007300 |
| inclination: | 97.7019° |
| perigee height: | 626 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 158.1359° |
| argument of perigee: | 33.8127° |
| revolutions per day: | 14.79469201 |
| mean anomaly at epoch: | 139.4567° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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