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 57648U 26145.37456654 +.00000000 +00000-0 +26524-4 0 00004
2 57648 43.0049 19.5360 0001947 259.9182 100.1450 15.27585950 01
| Epoch (UTC): | 25 May 2026 08:59:22 |
| Eccentricity: | 0.0001947 |
| inclination: | 43.0049° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 19.5360° |
| argument of perigee: | 259.9182° |
| revolutions per day: | 15.27585950 |
| mean anomaly at epoch: | 100.1450° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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