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 67185U 26145.61397352 +.00000000 +00000-0 +62621-3 0 00004
2 67185 42.9946 235.9421 0002210 277.9060 82.1541 15.27598886 05
| Epoch (UTC): | 25 May 2026 14:44:07 |
| Eccentricity: | 0.0002210 |
| inclination: | 42.9946° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 235.9421° |
| argument of perigee: | 277.9060° |
| revolutions per day: | 15.27598886 |
| mean anomaly at epoch: | 82.1541° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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