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 67842U 26145.44252323 +.00000000 +00000-0 +49507-3 0 00001
2 67842 43.0017 193.4802 0001273 271.3840 88.6866 15.27591197 08
| Epoch (UTC): | 25 May 2026 10:37:14 |
| Eccentricity: | 0.0001273 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 193.4802° |
| argument of perigee: | 271.3840° |
| revolutions per day: | 15.27591197 |
| mean anomaly at epoch: | 88.6866° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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