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 67563U 26145.14358672 +.00000000 +00000-0 +61780-3 0 00009
2 67563 97.2834 205.5133 0001513 76.9182 283.2229 15.33451544 07
| Epoch (UTC): | 25 May 2026 03:26:45 |
| Eccentricity: | 0.0001513 |
| inclination: | 97.2834° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 205.5133° |
| argument of perigee: | 76.9182° |
| revolutions per day: | 15.33451544 |
| mean anomaly at epoch: | 283.2229° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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