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 67057U 26145.46852465 +.00000000 +00000-0 +60187-3 0 00001
2 67057 42.9976 324.2838 0001044 275.7999 84.2734 15.27591700 06
| Epoch (UTC): | 25 May 2026 11:14:40 |
| Eccentricity: | 0.0001044 |
| inclination: | 42.9976° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 324.2838° |
| argument of perigee: | 275.7999° |
| revolutions per day: | 15.27591700 |
| mean anomaly at epoch: | 84.2734° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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