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 63454U 26145.37611035 +.00000000 +00000-0 +33108-3 0 00007
2 63454 53.1589 143.5687 0001205 79.2899 280.8243 15.42170173 09
| Epoch (UTC): | 25 May 2026 09:01:35 |
| Eccentricity: | 0.0001205 |
| inclination: | 53.1589° |
| perigee height: | 439 km |
| apogee height: | 441 km |
| right ascension of ascending node: | 143.5687° |
| argument of perigee: | 79.2899° |
| revolutions per day: | 15.42170173 |
| mean anomaly at epoch: | 280.8243° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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