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 67066U 26145.61945632 +.00000000 +00000-0 +86771-4 0 00005
2 67066 49.9980 106.1379 0000927 356.0534 4.0330 13.29327387 02
| Epoch (UTC): | 25 May 2026 14:52:01 |
| Eccentricity: | 0.0000927 |
| inclination: | 49.9980° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 106.1379° |
| argument of perigee: | 356.0534° |
| revolutions per day: | 13.29327387 |
| mean anomaly at epoch: | 4.0330° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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