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 68326U 26145.59442833 +.00000000 +00000-0 +73874-3 0 00006
2 68326 53.1578 350.7977 0000874 67.9180 292.1914 15.30205353 09
| Epoch (UTC): | 25 May 2026 14:15:58 |
| Eccentricity: | 0.0000874 |
| inclination: | 53.1578° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 350.7977° |
| argument of perigee: | 67.9180° |
| revolutions per day: | 15.30205353 |
| mean anomaly at epoch: | 292.1914° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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