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 26017.11944128 +.00000000 +00000-0 +61059-4 0 00009
2 23343 97.7169 50.0122 0007429 39.4331 27.3688 14.79335436 00
| Epoch (UTC): | 17 January 2026 02:51:59 |
| Eccentricity: | 0.0007429 |
| inclination: | 97.7169° |
| perigee height: | 626 km |
| apogee height: | 637 km |
| right ascension of ascending node: | 50.0122° |
| argument of perigee: | 39.4331° |
| revolutions per day: | 14.79335436 |
| mean anomaly at epoch: | 27.3688° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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