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 67845U 26145.49762698 +.00000000 +00000-0 +44393-3 0 00008
2 67845 43.0007 193.0235 0001453 276.4056 83.6630 15.27590015 03
| Epoch (UTC): | 25 May 2026 11:56:34 |
| Eccentricity: | 0.0001453 |
| inclination: | 43.0007° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 193.0235° |
| argument of perigee: | 276.4056° |
| revolutions per day: | 15.27590015 |
| mean anomaly at epoch: | 83.6630° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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