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 63446U 26145.32127667 +.00000000 +00000-0 +81764-3 0 00007
2 63446 53.1589 143.9521 0000995 67.7779 292.3333 15.42178845 07
| Epoch (UTC): | 25 May 2026 07:42:38 |
| Eccentricity: | 0.0000995 |
| inclination: | 53.1589° |
| perigee height: | 439 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 143.9521° |
| argument of perigee: | 67.7779° |
| revolutions per day: | 15.42178845 |
| mean anomaly at epoch: | 292.3333° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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