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 57242U 26145.49265919 +.00000000 +00000-0 +66898-4 0 00007
2 57242 42.9991 306.3577 0000290 246.1897 113.8924 15.27583921 06
| Epoch (UTC): | 25 May 2026 11:49:25 |
| Eccentricity: | 0.0000290 |
| inclination: | 42.9991° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 306.3577° |
| argument of perigee: | 246.1897° |
| revolutions per day: | 15.27583921 |
| mean anomaly at epoch: | 113.8924° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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