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 67826U 26145.44895794 +.00000000 +00000-0 +70102-3 0 00003
2 67826 43.0032 193.5300 0001678 285.2798 74.7868 15.27593049 02
| Epoch (UTC): | 25 May 2026 10:46:29 |
| Eccentricity: | 0.0001678 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 193.5300° |
| argument of perigee: | 285.2798° |
| revolutions per day: | 15.27593049 |
| mean anomaly at epoch: | 74.7868° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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