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 68832U 26145.43735931 +.00000000 +00000-0 +56340-3 0 00004
2 68832 55.0009 121.1094 0010866 3.3559 356.7531 15.19233787 08
| Epoch (UTC): | 25 May 2026 10:29:47 |
| Eccentricity: | 0.0010866 |
| inclination: | 55.0009° |
| perigee height: | 501 km |
| apogee height: | 516 km |
| right ascension of ascending node: | 121.1094° |
| argument of perigee: | 3.3559° |
| revolutions per day: | 15.19233787 |
| mean anomaly at epoch: | 356.7531° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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