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 67427U 26145.52186993 +.00000000 +00000-0 +16618-2 0 00004
2 67427 43.0011 164.3593 0001636 253.4419 106.6254 15.27612175 03
| Epoch (UTC): | 25 May 2026 12:31:29 |
| Eccentricity: | 0.0001636 |
| inclination: | 43.0011° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 164.3593° |
| argument of perigee: | 253.4419° |
| revolutions per day: | 15.27612175 |
| mean anomaly at epoch: | 106.6254° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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