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 67378U 26145.47356693 +.00000000 +00000-0 +72049-4 0 00001
2 67378 97.8006 144.3666 0002896 171.6713 188.4551 14.86316638 02
| Epoch (UTC): | 25 May 2026 11:21:56 |
| Eccentricity: | 0.0002896 |
| inclination: | 97.8006° |
| perigee height: | 607 km |
| apogee height: | 611 km |
| right ascension of ascending node: | 144.3666° |
| argument of perigee: | 171.6713° |
| revolutions per day: | 14.86316638 |
| mean anomaly at epoch: | 188.4551° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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