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 67438U 26145.32633470 +.00000000 +00000-0 +94483-4 0 00009
2 67438 50.0033 168.0245 0000869 281.6896 78.3879 13.29325087 02
| Epoch (UTC): | 25 May 2026 07:49:55 |
| Eccentricity: | 0.0000869 |
| inclination: | 50.0033° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 168.0245° |
| argument of perigee: | 281.6896° |
| revolutions per day: | 13.29325087 |
| mean anomaly at epoch: | 78.3879° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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