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 63355U 26145.37863748 +.00000000 +00000-0 +19230-3 0 00007
2 63355 97.5609 121.2197 0016352 344.8789 15.1952 15.13997425 02
| Epoch (UTC): | 25 May 2026 09:05:14 |
| Eccentricity: | 0.0016352 |
| inclination: | 97.5609° |
| perigee height: | 513 km |
| apogee height: | 535 km |
| right ascension of ascending node: | 121.2197° |
| argument of perigee: | 344.8789° |
| revolutions per day: | 15.13997425 |
| mean anomaly at epoch: | 15.1952° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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