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 63856U 26145.33662323 +.00000000 +00000-0 +50825-3 0 00000
2 63856 43.0040 5.0859 0001126 301.5103 58.5639 15.27594706 03
| Epoch (UTC): | 25 May 2026 08:04:44 |
| Eccentricity: | 0.0001126 |
| inclination: | 43.0040° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 5.0859° |
| argument of perigee: | 301.5103° |
| revolutions per day: | 15.27594706 |
| mean anomaly at epoch: | 58.5639° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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