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 67148U 26145.23783273 +.00000000 +00000-0 +46723-3 0 00007
2 67148 51.8991 87.1558 0001210 85.5967 274.5134 14.79890998 09
| Epoch (UTC): | 25 May 2026 05:42:28 |
| Eccentricity: | 0.0001210 |
| inclination: | 51.8991° |
| perigee height: | 629 km |
| apogee height: | 631 km |
| right ascension of ascending node: | 87.1558° |
| argument of perigee: | 85.5967° |
| revolutions per day: | 14.79890998 |
| mean anomaly at epoch: | 274.5134° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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