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 57457U 26145.38011183 +.00000000 +00000-0 +35761-4 0 00000
2 57457 43.0034 263.1951 0001732 263.7568 96.3087 15.27573808 00
| Epoch (UTC): | 25 May 2026 09:07:21 |
| Eccentricity: | 0.0001732 |
| inclination: | 43.0034° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 263.1951° |
| argument of perigee: | 263.7568° |
| revolutions per day: | 15.27573808 |
| mean anomaly at epoch: | 96.3087° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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