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 63959U 26145.19752317 +.00000000 +00000-0 +80252-3 0 00008
2 63959 43.0044 104.4558 0001745 272.0998 87.9653 15.27601818 07
| Epoch (UTC): | 25 May 2026 04:44:26 |
| Eccentricity: | 0.0001745 |
| inclination: | 43.0044° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 104.4558° |
| argument of perigee: | 272.0998° |
| revolutions per day: | 15.27601818 |
| mean anomaly at epoch: | 87.9653° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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