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 67060U 26145.28534529 +.00000000 +00000-0 +83739-4 0 00002
2 67060 50.0030 107.7813 0000834 356.3894 3.6972 13.29327329 07
| Epoch (UTC): | 25 May 2026 06:50:53 |
| Eccentricity: | 0.0000834 |
| inclination: | 50.0030° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 107.7813° |
| argument of perigee: | 356.3894° |
| revolutions per day: | 13.29327329 |
| mean anomaly at epoch: | 3.6972° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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