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 56553U 26145.44926139 +.00000000 +00000-0 +14656-4 0 00009
2 56553 43.0028 149.8977 0001055 311.1116 48.9645 15.27575656 08
| Epoch (UTC): | 25 May 2026 10:46:56 |
| Eccentricity: | 0.0001055 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 149.8977° |
| argument of perigee: | 311.1116° |
| revolutions per day: | 15.27575656 |
| mean anomaly at epoch: | 48.9645° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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