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 56535U 26145.43592222 +.00000000 +00000-0 -12105-3 0 00007
2 56535 43.0030 153.2169 0001246 262.4304 97.6406 15.27583762 05
| Epoch (UTC): | 25 May 2026 10:27:43 |
| Eccentricity: | 0.0001246 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 153.2169° |
| argument of perigee: | 262.4304° |
| revolutions per day: | 15.27583762 |
| mean anomaly at epoch: | 97.6406° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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