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 63656U 26145.43031102 +.00000000 +00000-0 +15255-2 0 00001
2 63656 42.9942 291.7880 0000608 329.0334 31.0482 15.27636152 07
| Epoch (UTC): | 25 May 2026 10:19:38 |
| Eccentricity: | 0.0000608 |
| inclination: | 42.9942° |
| perigee height: | 482 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 291.7880° |
| argument of perigee: | 329.0334° |
| revolutions per day: | 15.27636152 |
| mean anomaly at epoch: | 31.0482° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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