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 67054U 26145.54290516 +.00000000 +00000-0 +64770-3 0 00002
2 67054 42.9975 323.9834 0000146 38.1277 321.9585 15.27601003 09
| Epoch (UTC): | 25 May 2026 13:01:47 |
| Eccentricity: | 0.0000146 |
| inclination: | 42.9975° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 323.9834° |
| argument of perigee: | 38.1277° |
| revolutions per day: | 15.27601003 |
| mean anomaly at epoch: | 321.9585° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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