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 67348U 26145.33344903 +.00000000 +00000-0 +69461-3 0 00007
2 67348 43.0025 154.3899 0001596 265.9313 94.1357 15.27569661 00
| Epoch (UTC): | 25 May 2026 08:00:09 |
| Eccentricity: | 0.0001596 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 154.3899° |
| argument of perigee: | 265.9313° |
| revolutions per day: | 15.27569661 |
| mean anomaly at epoch: | 94.1357° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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