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 67382U 26144.95149830 +.00000000 +00000-0 +71780-4 0 00002
2 67382 97.8032 144.0102 0004380 174.6430 185.4835 14.88233864 00
| Epoch (UTC): | 24 May 2026 22:50:09 |
| Eccentricity: | 0.0004380 |
| inclination: | 97.8032° |
| perigee height: | 600 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 144.0102° |
| argument of perigee: | 174.6430° |
| revolutions per day: | 14.88233864 |
| mean anomaly at epoch: | 185.4835° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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