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 26039.58462735 +.00000000 +00000-0 +83038-4 0 00004
2 23343 97.7148 71.5762 0005664 327.3617 148.6707 14.79372664 03
| Epoch (UTC): | 08 February 2026 14:01:51 |
| Eccentricity: | 0.0005664 |
| inclination: | 97.7148° |
| perigee height: | 627 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 71.5762° |
| argument of perigee: | 327.3617° |
| revolutions per day: | 14.79372664 |
| mean anomaly at epoch: | 148.6707° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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