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 63439U 26145.29416594 +.00000000 +00000-0 +75421-3 0 00008
2 63439 53.1584 143.7862 0001180 85.0880 275.0261 15.42182648 07
| Epoch (UTC): | 25 May 2026 07:03:35 |
| Eccentricity: | 0.0001180 |
| inclination: | 53.1584° |
| perigee height: | 439 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 143.7862° |
| argument of perigee: | 85.0880° |
| revolutions per day: | 15.42182648 |
| mean anomaly at epoch: | 275.0261° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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