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 57906U 26144.67383750 +.00000000 +00000-0 +48794-4 0 00002
2 57906 43.0035 245.3690 0001588 264.4756 95.5915 15.27578518 02
| Epoch (UTC): | 24 May 2026 16:10:19 |
| Eccentricity: | 0.0001588 |
| inclination: | 43.0035° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 245.3690° |
| argument of perigee: | 264.4756° |
| revolutions per day: | 15.27578518 |
| mean anomaly at epoch: | 95.5915° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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