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 67186U 26145.30246615 +.00000000 +00000-0 +64917-3 0 00006
2 67186 42.9971 237.9053 0000916 211.4949 148.5848 15.27593664 03
| Epoch (UTC): | 25 May 2026 07:15:33 |
| Eccentricity: | 0.0000916 |
| inclination: | 42.9971° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 237.9053° |
| argument of perigee: | 211.4949° |
| revolutions per day: | 15.27593664 |
| mean anomaly at epoch: | 148.5848° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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