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 63226U 26145.28185456 +.00000000 +00000-0 +16214-3 0 00006
2 63226 97.3991 38.1958 0004155 204.3953 155.7087 15.21891180 03
| Epoch (UTC): | 25 May 2026 06:45:52 |
| Eccentricity: | 0.0004155 |
| inclination: | 97.3991° |
| perigee height: | 497 km |
| apogee height: | 503 km |
| right ascension of ascending node: | 38.1958° |
| argument of perigee: | 204.3953° |
| revolutions per day: | 15.21891180 |
| mean anomaly at epoch: | 155.7087° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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