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 26474U 26042.25739193 +.00000000 +00000-0 +22848-3 0 00006
2 26474 67.9889 114.8251 0037047 67.8464 292.6611 15.09339238 00
| Epoch (UTC): | 11 February 2026 06:10:38 |
| Eccentricity: | 0.0037047 |
| inclination: | 67.9889° |
| perigee height: | 513 km |
| apogee height: | 564 km |
| right ascension of ascending node: | 114.8251° |
| argument of perigee: | 67.8464° |
| revolutions per day: | 15.09339238 |
| mean anomaly at epoch: | 292.6611° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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