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 26071.71335811 +.00000000 +00000-0 +86804-4 0 00003
2 23343 97.7106 102.4086 0006035 199.4350 283.4668 14.79412069 03
| Epoch (UTC): | 12 March 2026 17:07:14 |
| Eccentricity: | 0.0006035 |
| inclination: | 97.7106° |
| perigee height: | 627 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 102.4086° |
| argument of perigee: | 199.4350° |
| revolutions per day: | 14.79412069 |
| mean anomaly at epoch: | 283.4668° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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