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 47754U 26145.66668980 +.00000000 +00000-0 +82225-3 0 00009
2 47754 53.0327 140.7590 0009750 42.6608 310.7303 15.99513959 05
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0009750 |
| inclination: | 53.0327° |
| perigee height: | 269 km |
| apogee height: | 282 km |
| right ascension of ascending node: | 140.7590° |
| argument of perigee: | 42.6608° |
| revolutions per day: | 15.99513959 |
| mean anomaly at epoch: | 310.7303° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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