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 26134.32159450 +.00000000 +00000-0 +42599-4 0 00006
2 23343 97.7015 162.4505 0006936 20.4743 349.9706 14.79472186 00
| Epoch (UTC): | 14 May 2026 07:43:05 |
| Eccentricity: | 0.0006936 |
| inclination: | 97.7015° |
| perigee height: | 626 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 162.4505° |
| argument of perigee: | 20.4743° |
| revolutions per day: | 14.79472186 |
| mean anomaly at epoch: | 349.9706° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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