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 67387U 26145.59018350 +.00000000 +00000-0 +29317-3 0 00008
2 67387 97.8038 144.8894 0003831 139.9571 220.1930 14.89864392 07
| Epoch (UTC): | 25 May 2026 14:09:51 |
| Eccentricity: | 0.0003831 |
| inclination: | 97.8038° |
| perigee height: | 596 km |
| apogee height: | 601 km |
| right ascension of ascending node: | 144.8894° |
| argument of perigee: | 139.9571° |
| revolutions per day: | 14.89864392 |
| mean anomaly at epoch: | 220.1930° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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