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 63909U 26145.37057385 +.00000000 +00000-0 +59882-3 0 00001
2 63909 42.9996 103.2934 0001176 269.0357 91.0360 15.27594675 07
| Epoch (UTC): | 25 May 2026 08:53:37 |
| Eccentricity: | 0.0001176 |
| inclination: | 42.9996° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 103.2934° |
| argument of perigee: | 269.0357° |
| revolutions per day: | 15.27594675 |
| mean anomaly at epoch: | 91.0360° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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