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 63911U 26145.36286306 +.00000000 +00000-0 +57898-3 0 00005
2 63911 43.0014 103.2329 0001778 274.6733 85.3915 15.27601735 07
| Epoch (UTC): | 25 May 2026 08:42:31 |
| Eccentricity: | 0.0001778 |
| inclination: | 43.0014° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 103.2329° |
| argument of perigee: | 274.6733° |
| revolutions per day: | 15.27601735 |
| mean anomaly at epoch: | 85.3915° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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