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 63200U 26144.92029240 +.00000000 +00000-0 +88232-3 0 00005
2 63200 42.9998 14.5487 0001075 272.1553 87.9176 15.27595330 09
| Epoch (UTC): | 24 May 2026 22:05:13 |
| Eccentricity: | 0.0001075 |
| inclination: | 42.9998° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 14.5487° |
| argument of perigee: | 272.1553° |
| revolutions per day: | 15.27595330 |
| mean anomaly at epoch: | 87.9176° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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