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 69081U 26144.83915019 +.00000000 +00000-0 +28174-4 0 00006
2 69081 88.9870 344.2879 0002775 191.4733 168.6395 14.20302891 00
| Epoch (UTC): | 24 May 2026 20:08:22 |
| Eccentricity: | 0.0002775 |
| inclination: | 88.9870° |
| perigee height: | 822 km |
| apogee height: | 826 km |
| right ascension of ascending node: | 344.2879° |
| argument of perigee: | 191.4733° |
| revolutions per day: | 14.20302891 |
| mean anomaly at epoch: | 168.6395° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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