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 25544U 26131.68281699 +.00000000 +00000-0 +99294-4 0 00002
2 25544 51.6311 120.8028 0007472 48.2126 311.9500 15.49186980 03
| Epoch (UTC): | 11 May 2026 16:23:15 |
| Eccentricity: | 0.0007472 |
| inclination: | 51.6311° |
| perigee height: | 414 km |
| apogee height: | 424 km |
| right ascension of ascending node: | 120.8028° |
| argument of perigee: | 48.2126° |
| revolutions per day: | 15.49186980 |
| mean anomaly at epoch: | 311.9500° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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