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 67406U 26145.44492377 +.00000000 +00000-0 +86360-3 0 00000
2 67406 43.0051 164.6517 0002615 260.0364 100.0193 15.27541932 06
| Epoch (UTC): | 25 May 2026 10:40:41 |
| Eccentricity: | 0.0002615 |
| inclination: | 43.0051° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 164.6517° |
| argument of perigee: | 260.0364° |
| revolutions per day: | 15.27541932 |
| mean anomaly at epoch: | 100.0193° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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