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 63348U 26145.57888600 +.00000000 +00000-0 +20236-3 0 00003
2 63348 97.6091 327.1032 0014824 232.3905 127.5979 15.11027003 09
| Epoch (UTC): | 25 May 2026 13:53:35 |
| Eccentricity: | 0.0014824 |
| inclination: | 97.6091° |
| perigee height: | 523 km |
| apogee height: | 543 km |
| right ascension of ascending node: | 327.1032° |
| argument of perigee: | 232.3905° |
| revolutions per day: | 15.11027003 |
| mean anomaly at epoch: | 127.5979° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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