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 67413U 26145.48074366 +.00000000 +00000-0 +48492-3 0 00000
2 67413 42.9988 164.0538 0001247 266.1904 93.8805 15.27588356 05
| Epoch (UTC): | 25 May 2026 11:32:16 |
| Eccentricity: | 0.0001247 |
| inclination: | 42.9988° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 164.0538° |
| argument of perigee: | 266.1904° |
| revolutions per day: | 15.27588356 |
| mean anomaly at epoch: | 93.8805° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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