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 63954U 26145.26932416 +.00000000 +00000-0 +21615-4 0 00000
2 63954 43.0014 104.1341 0001248 267.0019 93.0690 15.27581843 06
| Epoch (UTC): | 25 May 2026 06:27:49 |
| Eccentricity: | 0.0001248 |
| inclination: | 43.0014° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 104.1341° |
| argument of perigee: | 267.0019° |
| revolutions per day: | 15.27581843 |
| mean anomaly at epoch: | 93.0690° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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