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 55464U 26144.74248581 +.00000000 +00000-0 -14159-4 0 00008
2 55464 43.0020 259.1852 0001285 269.7449 90.3255 15.27571009 05
| Epoch (UTC): | 24 May 2026 17:49:10 |
| Eccentricity: | 0.0001285 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 259.1852° |
| argument of perigee: | 269.7449° |
| revolutions per day: | 15.27571009 |
| mean anomaly at epoch: | 90.3255° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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