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 67841U 26145.44637426 +.00000000 +00000-0 +72928-3 0 00004
2 67841 43.0060 193.5084 0002909 275.2008 84.8511 15.27606503 07
| Epoch (UTC): | 25 May 2026 10:42:46 |
| Eccentricity: | 0.0002909 |
| inclination: | 43.0060° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 193.5084° |
| argument of perigee: | 275.2008° |
| revolutions per day: | 15.27606503 |
| mean anomaly at epoch: | 84.8511° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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