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 26132.19887559 +.00000000 +00000-0 +93039-4 0 00007
2 25544 51.6312 118.2489 0007476 49.7974 310.3668 15.49191856 03
| Epoch (UTC): | 12 May 2026 04:46:22 |
| Eccentricity: | 0.0007476 |
| inclination: | 51.6312° |
| perigee height: | 414 km |
| apogee height: | 424 km |
| right ascension of ascending node: | 118.2489° |
| argument of perigee: | 49.7974° |
| revolutions per day: | 15.49191856 |
| mean anomaly at epoch: | 310.3668° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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