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 67088U 26145.60151676 +.00000000 +00000-0 +18697-3 0 00006
2 67088 70.0006 180.7047 0004637 264.5719 95.4912 14.98334946 06
| Epoch (UTC): | 25 May 2026 14:26:11 |
| Eccentricity: | 0.0004637 |
| inclination: | 70.0006° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 180.7047° |
| argument of perigee: | 264.5719° |
| revolutions per day: | 14.98334946 |
| mean anomaly at epoch: | 95.4912° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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