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 63644U 26145.12393163 +.00000000 +00000-0 +90365-3 0 00008
2 63644 42.9957 293.8006 0000702 297.0456 63.0324 15.27581746 05
| Epoch (UTC): | 25 May 2026 02:58:27 |
| Eccentricity: | 0.0000702 |
| inclination: | 42.9957° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 293.8006° |
| argument of perigee: | 297.0456° |
| revolutions per day: | 15.27581746 |
| mean anomaly at epoch: | 63.0324° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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