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 63952U 26145.26162531 +.00000000 +00000-0 +23226-3 0 00000
2 63952 43.0019 104.0780 0000970 269.9748 90.0992 15.27584573 01
| Epoch (UTC): | 25 May 2026 06:16:44 |
| Eccentricity: | 0.0000970 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 104.0780° |
| argument of perigee: | 269.9748° |
| revolutions per day: | 15.27584573 |
| mean anomaly at epoch: | 90.0992° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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