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 67410U 26145.39751550 +.00000000 +00000-0 +70500-3 0 00009
2 67410 43.0005 165.1537 0001688 270.0419 90.0239 15.27601144 00
| Epoch (UTC): | 25 May 2026 09:32:25 |
| Eccentricity: | 0.0001688 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 165.1537° |
| argument of perigee: | 270.0419° |
| revolutions per day: | 15.27601144 |
| mean anomaly at epoch: | 90.0239° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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