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 67305U 26145.59294766 +.00000000 +00000-0 +53342-3 0 00000
2 67305 43.0019 250.6659 0000651 37.9436 322.1462 15.27590218 07
| Epoch (UTC): | 25 May 2026 14:13:50 |
| Eccentricity: | 0.0000651 |
| inclination: | 43.0019° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 250.6659° |
| argument of perigee: | 37.9436° |
| revolutions per day: | 15.27590218 |
| mean anomaly at epoch: | 322.1462° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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