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 63966U 26145.35256281 +.00000000 +00000-0 +41571-3 0 00004
2 63966 43.0016 103.0262 0001621 270.2183 89.8483 15.27588794 09
| Epoch (UTC): | 25 May 2026 08:27:41 |
| Eccentricity: | 0.0001621 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 103.0262° |
| argument of perigee: | 270.2183° |
| revolutions per day: | 15.27588794 |
| mean anomaly at epoch: | 89.8483° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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