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 67478U 26145.46961145 +.00000000 +00000-0 +12210-3 0 00008
2 67478 44.9804 179.8566 0016071 234.1912 125.7429 14.03969419 08
| Epoch (UTC): | 25 May 2026 11:16:14 |
| Eccentricity: | 0.0016071 |
| inclination: | 44.9804° |
| perigee height: | 868 km |
| apogee height: | 892 km |
| right ascension of ascending node: | 179.8566° |
| argument of perigee: | 234.1912° |
| revolutions per day: | 14.03969419 |
| mean anomaly at epoch: | 125.7429° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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