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 63451U 26145.39375907 +.00000000 +00000-0 +60463-3 0 00005
2 63451 53.1593 143.6919 0001474 89.3375 270.7800 15.42179829 03
| Epoch (UTC): | 25 May 2026 09:27:00 |
| Eccentricity: | 0.0001474 |
| inclination: | 53.1593° |
| perigee height: | 439 km |
| apogee height: | 441 km |
| right ascension of ascending node: | 143.6919° |
| argument of perigee: | 89.3375° |
| revolutions per day: | 15.42179829 |
| mean anomaly at epoch: | 270.7800° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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