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 63590U 26145.56787502 +.00000000 +00000-0 +67673-3 0 00006
2 63590 42.9988 247.8848 0000690 262.6806 97.3968 15.27579356 03
| Epoch (UTC): | 25 May 2026 13:37:44 |
| Eccentricity: | 0.0000690 |
| inclination: | 42.9988° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 247.8848° |
| argument of perigee: | 262.6806° |
| revolutions per day: | 15.27579356 |
| mean anomaly at epoch: | 97.3968° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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