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 67825U 26145.42324779 +.00000000 +00000-0 +41588-3 0 00006
2 67825 42.9998 193.3247 0001255 277.0576 83.0133 15.27580103 07
| Epoch (UTC): | 25 May 2026 10:09:28 |
| Eccentricity: | 0.0001255 |
| inclination: | 42.9998° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 193.3247° |
| argument of perigee: | 277.0576° |
| revolutions per day: | 15.27580103 |
| mean anomaly at epoch: | 83.0133° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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