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 56555U 26145.37359681 +.00000000 +00000-0 -40464-5 0 00003
2 56555 43.0000 150.1920 0001693 272.4543 87.6115 15.27575405 08
| Epoch (UTC): | 25 May 2026 08:57:58 |
| Eccentricity: | 0.0001693 |
| inclination: | 43.0000° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 150.1920° |
| argument of perigee: | 272.4543° |
| revolutions per day: | 15.27575405 |
| mean anomaly at epoch: | 87.6115° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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