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 67136U 26145.54173918 +.00000000 +00000-0 +13891-3 0 00007
2 67136 51.8968 85.7566 0000699 93.3055 266.7987 14.79932814 01
| Epoch (UTC): | 25 May 2026 13:00:06 |
| Eccentricity: | 0.0000699 |
| inclination: | 51.8968° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 85.7566° |
| argument of perigee: | 93.3055° |
| revolutions per day: | 14.79932814 |
| mean anomaly at epoch: | 266.7987° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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