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 67831U 26145.15542832 +.00000000 +00000-0 +41698-3 0 00007
2 67831 42.9994 195.6403 0001257 277.5447 82.5262 15.27587980 00
| Epoch (UTC): | 25 May 2026 03:43:49 |
| Eccentricity: | 0.0001257 |
| inclination: | 42.9994° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 195.6403° |
| argument of perigee: | 277.5447° |
| revolutions per day: | 15.27587980 |
| mean anomaly at epoch: | 82.5262° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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