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 69088U 26144.96574198 +.00000000 +00000-0 +30797-4 0 00000
2 69088 88.9871 344.2660 0003550 136.1326 224.0148 14.23303746 08
| Epoch (UTC): | 24 May 2026 23:10:40 |
| Eccentricity: | 0.0003550 |
| inclination: | 88.9871° |
| perigee height: | 812 km |
| apogee height: | 817 km |
| right ascension of ascending node: | 344.2660° |
| argument of perigee: | 136.1326° |
| revolutions per day: | 14.23303746 |
| mean anomaly at epoch: | 224.0148° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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