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 26069.49164611 +.00000000 +00000-0 +34475-3 0 00007
2 26474 67.9902 38.2551 0038655 34.4661 325.8983 15.09572482 04
| Epoch (UTC): | 10 March 2026 11:47:58 |
| Eccentricity: | 0.0038655 |
| inclination: | 67.9902° |
| perigee height: | 511 km |
| apogee height: | 564 km |
| right ascension of ascending node: | 38.2551° |
| argument of perigee: | 34.4661° |
| revolutions per day: | 15.09572482 |
| mean anomaly at epoch: | 325.8983° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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