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 67462U 26145.32843720 +.00000000 +00000-0 +66628-3 0 00006
2 67462 43.0008 132.3571 0000979 266.1589 93.9151 15.27597561 02
| Epoch (UTC): | 25 May 2026 07:52:56 |
| Eccentricity: | 0.0000979 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 132.3571° |
| argument of perigee: | 266.1589° |
| revolutions per day: | 15.27597561 |
| mean anomaly at epoch: | 93.9151° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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