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 67469U 26145.35541664 +.00000000 +00000-0 +58187-3 0 00009
2 67469 43.0044 132.5612 0002929 269.6681 90.3835 15.27601477 07
| Epoch (UTC): | 25 May 2026 08:31:47 |
| Eccentricity: | 0.0002929 |
| inclination: | 43.0044° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 132.5612° |
| argument of perigee: | 269.6681° |
| revolutions per day: | 15.27601477 |
| mean anomaly at epoch: | 90.3835° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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