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 67823U 26145.45151644 +.00000000 +00000-0 +47489-3 0 00002
2 67823 43.0043 193.5536 0001647 270.7739 89.2924 15.27591771 06
| Epoch (UTC): | 25 May 2026 10:50:11 |
| Eccentricity: | 0.0001647 |
| inclination: | 43.0043° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 193.5536° |
| argument of perigee: | 270.7739° |
| revolutions per day: | 15.27591771 |
| mean anomaly at epoch: | 89.2924° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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