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 67084U 26145.53059779 +.00000000 +00000-0 +29345-3 0 00007
2 67084 70.0012 180.8590 0003328 268.6073 91.4704 14.98338373 00
| Epoch (UTC): | 25 May 2026 12:44:03 |
| Eccentricity: | 0.0003328 |
| inclination: | 70.0012° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 180.8590° |
| argument of perigee: | 268.6073° |
| revolutions per day: | 14.98338373 |
| mean anomaly at epoch: | 91.4704° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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