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 67934U 26145.23548051 +.00000000 +00000-0 +18012-3 0 00003
2 67934 43.0013 118.7607 0002054 286.5826 73.4800 15.27493898 08
| Epoch (UTC): | 25 May 2026 05:39:05 |
| Eccentricity: | 0.0002054 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 118.7607° |
| argument of perigee: | 286.5826° |
| revolutions per day: | 15.27493898 |
| mean anomaly at epoch: | 73.4800° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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