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 26132.45690432 +.00000000 +00000-0 +95300-4 0 00001
2 25544 51.6310 116.9716 0007499 50.7815 309.3838 15.49194663 06
| Epoch (UTC): | 12 May 2026 10:57:56 |
| Eccentricity: | 0.0007499 |
| inclination: | 51.6310° |
| perigee height: | 414 km |
| apogee height: | 424 km |
| right ascension of ascending node: | 116.9716° |
| argument of perigee: | 50.7815° |
| revolutions per day: | 15.49194663 |
| mean anomaly at epoch: | 309.3838° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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