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 67955U 26145.27642067 +.00000000 +00000-0 +95950-3 0 00008
2 67955 42.9986 118.1927 0001485 269.8996 90.1685 15.27598300 07
| Epoch (UTC): | 25 May 2026 06:38:02 |
| Eccentricity: | 0.0001485 |
| inclination: | 42.9986° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 118.1927° |
| argument of perigee: | 269.8996° |
| revolutions per day: | 15.27598300 |
| mean anomaly at epoch: | 90.1685° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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