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 56532U 26145.31914715 +.00000000 +00000-0 +14234-4 0 00001
2 56532 43.0024 125.4706 0000976 281.5762 78.4980 15.27577166 07
| Epoch (UTC): | 25 May 2026 07:39:34 |
| Eccentricity: | 0.0000976 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 125.4706° |
| argument of perigee: | 281.5762° |
| revolutions per day: | 15.27577166 |
| mean anomaly at epoch: | 78.4980° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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