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 67405U 26145.34228992 +.00000000 +00000-0 +82822-3 0 00007
2 67405 42.9973 164.7343 0000799 277.4235 82.6526 15.27521200 05
| Epoch (UTC): | 25 May 2026 08:12:53 |
| Eccentricity: | 0.0000799 |
| inclination: | 42.9973° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 164.7343° |
| argument of perigee: | 277.4235° |
| revolutions per day: | 15.27521200 |
| mean anomaly at epoch: | 82.6526° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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