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 67388U 26145.38766094 +.00000000 +00000-0 +45638-3 0 00005
2 67388 97.8026 144.6739 0003589 133.7116 226.4399 14.89825736 05
| Epoch (UTC): | 25 May 2026 09:18:13 |
| Eccentricity: | 0.0003589 |
| inclination: | 97.8026° |
| perigee height: | 596 km |
| apogee height: | 601 km |
| right ascension of ascending node: | 144.6739° |
| argument of perigee: | 133.7116° |
| revolutions per day: | 14.89825736 |
| mean anomaly at epoch: | 226.4399° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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