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 57446U 26145.46402773 +.00000000 +00000-0 -10877-4 0 00008
2 57446 43.0032 175.2142 0001203 274.4190 85.6525 15.27582066 08
| Epoch (UTC): | 25 May 2026 11:08:11 |
| Eccentricity: | 0.0001203 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 175.2142° |
| argument of perigee: | 274.4190° |
| revolutions per day: | 15.27582066 |
| mean anomaly at epoch: | 85.6525° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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