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 57475U 26144.75051285 +.00000000 +00000-0 +21618-4 0 00003
2 57475 43.0015 266.2076 0001744 262.5940 97.4713 15.27577659 01
| Epoch (UTC): | 24 May 2026 18:00:44 |
| Eccentricity: | 0.0001744 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 266.2076° |
| argument of perigee: | 262.5940° |
| revolutions per day: | 15.27577659 |
| mean anomaly at epoch: | 97.4713° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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