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 67450U 26145.27333492 +.00000000 +00000-0 +87579-3 0 00005
2 67450 42.9966 132.8106 0001101 281.3426 78.7302 15.27587150 08
| Epoch (UTC): | 25 May 2026 06:33:36 |
| Eccentricity: | 0.0001101 |
| inclination: | 42.9966° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 132.8106° |
| argument of perigee: | 281.3426° |
| revolutions per day: | 15.27587150 |
| mean anomaly at epoch: | 78.7302° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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