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 56556U 26145.45311632 +.00000000 +00000-0 +23187-4 0 00008
2 56556 43.0025 149.9303 0001266 312.5388 47.5357 15.27577082 02
| Epoch (UTC): | 25 May 2026 10:52:29 |
| Eccentricity: | 0.0001266 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 149.9303° |
| argument of perigee: | 312.5388° |
| revolutions per day: | 15.27577082 |
| mean anomaly at epoch: | 47.5357° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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