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 57607U 26145.26611507 +.00000000 +00000-0 +40303-4 0 00008
2 57607 43.0032 354.1744 0001192 278.3839 81.6878 15.27578001 04
| Epoch (UTC): | 25 May 2026 06:23:12 |
| Eccentricity: | 0.0001192 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 354.1744° |
| argument of perigee: | 278.3839° |
| revolutions per day: | 15.27578001 |
| mean anomaly at epoch: | 81.6878° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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