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 67843U 26145.43481301 +.00000000 +00000-0 +66927-3 0 00006
2 67843 42.9998 193.4194 0000653 248.1073 111.9709 15.27582348 04
| Epoch (UTC): | 25 May 2026 10:26:07 |
| Eccentricity: | 0.0000653 |
| inclination: | 42.9998° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 193.4194° |
| argument of perigee: | 248.1073° |
| revolutions per day: | 15.27582348 |
| mean anomaly at epoch: | 111.9709° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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