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 26073.05305207 +.00000000 +00000-0 +78342-4 0 00006
2 23343 97.7103 103.6941 0006094 194.8036 218.7919 14.79413545 08
| Epoch (UTC): | 14 March 2026 01:16:23 |
| Eccentricity: | 0.0006094 |
| inclination: | 97.7103° |
| perigee height: | 627 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 103.6941° |
| argument of perigee: | 194.8036° |
| revolutions per day: | 14.79413545 |
| mean anomaly at epoch: | 218.7919° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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