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 40544U 26144.16294227 +.00000000 +00000-0 +00000-0 0 00000
2 40544 56.7947 342.2501 0002259 291.5829 68.4129 1.70476041 08
| Epoch (UTC): | 24 May 2026 03:54:38 |
| Eccentricity: | 0.0002259 |
| inclination: | 56.7947° |
| perigee height: | 23215 km |
| apogee height: | 23229 km |
| right ascension of ascending node: | 342.2501° |
| argument of perigee: | 291.5829° |
| revolutions per day: | 1.70476041 |
| mean anomaly at epoch: | 68.4129° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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