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 26074.92465676 +.00000000 +00000-0 +26163-3 0 00001
2 26474 67.9907 22.9766 0038748 27.9844 332.3377 15.09628971 05
| Epoch (UTC): | 15 March 2026 22:11:30 |
| Eccentricity: | 0.0038748 |
| inclination: | 67.9907° |
| perigee height: | 511 km |
| apogee height: | 564 km |
| right ascension of ascending node: | 22.9766° |
| argument of perigee: | 27.9844° |
| revolutions per day: | 15.09628971 |
| mean anomaly at epoch: | 332.3377° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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