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 67189U 26145.53588897 +.00000000 +00000-0 +54580-3 0 00000
2 67189 43.0004 237.0841 0000328 258.9991 101.0824 15.27587486 04
| Epoch (UTC): | 25 May 2026 12:51:40 |
| Eccentricity: | 0.0000328 |
| inclination: | 43.0004° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 237.0841° |
| argument of perigee: | 258.9991° |
| revolutions per day: | 15.27587486 |
| mean anomaly at epoch: | 101.0824° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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