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 67073U 26145.65550146 +.00000000 +00000-0 +20184-3 0 00004
2 67073 97.5089 294.1957 0013915 112.5472 247.7231 15.08818326 09
| Epoch (UTC): | 25 May 2026 15:43:55 |
| Eccentricity: | 0.0013915 |
| inclination: | 97.5089° |
| perigee height: | 530 km |
| apogee height: | 549 km |
| right ascension of ascending node: | 294.1957° |
| argument of perigee: | 112.5472° |
| revolutions per day: | 15.08818326 |
| mean anomaly at epoch: | 247.7231° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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