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 67530U 26145.53834285 +.00000000 +00000-0 +62369-4 0 00000
2 67530 50.0069 76.5184 0000925 28.2263 331.8660 13.29328188 05
| Epoch (UTC): | 25 May 2026 12:55:12 |
| Eccentricity: | 0.0000925 |
| inclination: | 50.0069° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 76.5184° |
| argument of perigee: | 28.2263° |
| revolutions per day: | 13.29328188 |
| mean anomaly at epoch: | 331.8660° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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