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 63426U 26144.98047559 +.00000000 +00000-0 +57032-3 0 00008
2 63426 43.0001 36.5124 0000823 253.0264 107.0498 15.27596520 08
| Epoch (UTC): | 24 May 2026 23:31:53 |
| Eccentricity: | 0.0000823 |
| inclination: | 43.0001° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 36.5124° |
| argument of perigee: | 253.0264° |
| revolutions per day: | 15.27596520 |
| mean anomaly at epoch: | 107.0498° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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