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 57133U 26145.44938319 +.00000000 +00000-0 +29799-4 0 00001
2 57133 43.0032 189.7751 0001868 276.9826 83.0813 15.27576844 06
| Epoch (UTC): | 25 May 2026 10:47:06 |
| Eccentricity: | 0.0001868 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 189.7751° |
| argument of perigee: | 276.9826° |
| revolutions per day: | 15.27576844 |
| mean anomaly at epoch: | 83.0813° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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