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 67391U 26144.94757344 +.00000000 +00000-0 +78064-4 0 00008
2 67391 97.4545 144.2162 0006430 59.2043 300.9823 15.17719502 01
| Epoch (UTC): | 24 May 2026 22:44:30 |
| Eccentricity: | 0.0006430 |
| inclination: | 97.4545° |
| perigee height: | 508 km |
| apogee height: | 517 km |
| right ascension of ascending node: | 144.2162° |
| argument of perigee: | 59.2043° |
| revolutions per day: | 15.17719502 |
| mean anomaly at epoch: | 300.9823° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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