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 67425U 26145.36411730 +.00000000 +00000-0 +18998-3 0 00008
2 67425 43.0004 164.8984 0001910 280.1127 79.9509 15.27575542 01
| Epoch (UTC): | 25 May 2026 08:44:19 |
| Eccentricity: | 0.0001910 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 164.8984° |
| argument of perigee: | 280.1127° |
| revolutions per day: | 15.27575542 |
| mean anomaly at epoch: | 79.9509° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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