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 67182U 26145.28576150 +.00000000 +00000-0 +84085-3 0 00007
2 67182 42.9957 237.7830 0000403 329.3633 30.7195 15.27590095 06
| Epoch (UTC): | 25 May 2026 06:51:29 |
| Eccentricity: | 0.0000403 |
| inclination: | 42.9957° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 237.7830° |
| argument of perigee: | 329.3633° |
| revolutions per day: | 15.27590095 |
| mean anomaly at epoch: | 30.7195° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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