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 63497U 26145.27600249 +.00000000 +00000-0 +37756-3 0 00001
2 63497 53.1589 144.3314 0001111 78.5714 281.5412 15.31712243 00
| Epoch (UTC): | 25 May 2026 06:37:26 |
| Eccentricity: | 0.0001111 |
| inclination: | 53.1589° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 144.3314° |
| argument of perigee: | 78.5714° |
| revolutions per day: | 15.31712243 |
| mean anomaly at epoch: | 281.5412° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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