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 63351U 26145.54223418 +.00000000 +00000-0 +21583-3 0 00000
2 63351 97.5625 121.0744 0018423 349.0429 11.0398 15.13287817 07
| Epoch (UTC): | 25 May 2026 13:00:49 |
| Eccentricity: | 0.0018423 |
| inclination: | 97.5625° |
| perigee height: | 513 km |
| apogee height: | 539 km |
| right ascension of ascending node: | 121.0744° |
| argument of perigee: | 349.0429° |
| revolutions per day: | 15.13287817 |
| mean anomaly at epoch: | 11.0398° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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