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 67361U 26145.44623411 +.00000000 +00000-0 +59299-3 0 00006
2 67361 43.0008 153.5124 0001480 270.0983 89.9699 15.27588779 02
| Epoch (UTC): | 25 May 2026 10:42:34 |
| Eccentricity: | 0.0001480 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 153.5124° |
| argument of perigee: | 270.0983° |
| revolutions per day: | 15.27588779 |
| mean anomaly at epoch: | 89.9699° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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