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 67241U 26145.43245465 +.00000000 +00000-0 +73509-4 0 00002
2 67241 50.0089 197.3951 0000970 247.0904 112.9866 13.29323059 01
| Epoch (UTC): | 25 May 2026 10:22:44 |
| Eccentricity: | 0.0000970 |
| inclination: | 50.0089° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 197.3951° |
| argument of perigee: | 247.0904° |
| revolutions per day: | 13.29323059 |
| mean anomaly at epoch: | 112.9866° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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