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 67326U 26145.32240234 +.00000000 +00000-0 +70171-3 0 00004
2 67326 42.9961 252.0700 0000551 293.2522 66.8272 15.27594563 07
| Epoch (UTC): | 25 May 2026 07:44:15 |
| Eccentricity: | 0.0000551 |
| inclination: | 42.9961° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 252.0700° |
| argument of perigee: | 293.2522° |
| revolutions per day: | 15.27594563 |
| mean anomaly at epoch: | 66.8272° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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