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 67110U 26145.13048240 +.00000000 +00000-0 +57430-3 0 00000
2 67110 43.0010 97.5723 0001469 263.8142 96.2542 15.27590979 06
| Epoch (UTC): | 25 May 2026 03:07:53 |
| Eccentricity: | 0.0001469 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 97.5723° |
| argument of perigee: | 263.8142° |
| revolutions per day: | 15.27590979 |
| mean anomaly at epoch: | 96.2542° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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