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 63358U 26145.48133863 +.00000000 +00000-0 +23035-3 0 00008
2 63358 97.5601 121.3417 0016157 342.5697 17.4978 15.14091664 03
| Epoch (UTC): | 25 May 2026 11:33:07 |
| Eccentricity: | 0.0016157 |
| inclination: | 97.5601° |
| perigee height: | 513 km |
| apogee height: | 535 km |
| right ascension of ascending node: | 121.3417° |
| argument of perigee: | 342.5697° |
| revolutions per day: | 15.14091664 |
| mean anomaly at epoch: | 17.4978° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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