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 67349U 26145.44880644 +.00000000 +00000-0 +38587-3 0 00002
2 67349 43.0002 153.5340 0001230 261.2133 98.8580 15.27580736 07
| Epoch (UTC): | 25 May 2026 10:46:16 |
| Eccentricity: | 0.0001230 |
| inclination: | 43.0002° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 153.5340° |
| argument of perigee: | 261.2133° |
| revolutions per day: | 15.27580736 |
| mean anomaly at epoch: | 98.8580° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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