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 67463U 26145.32460699 +.00000000 +00000-0 +61460-3 0 00006
2 67463 42.9995 132.3292 0000963 275.9017 84.1725 15.27582651 06
| Epoch (UTC): | 25 May 2026 07:47:26 |
| Eccentricity: | 0.0000963 |
| inclination: | 42.9995° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 132.3292° |
| argument of perigee: | 275.9017° |
| revolutions per day: | 15.27582651 |
| mean anomaly at epoch: | 84.1725° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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