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 67440U 26145.43492306 +.00000000 +00000-0 +95433-4 0 00001
2 67440 50.0099 167.3478 0000872 283.3958 76.6817 13.29325295 03
| Epoch (UTC): | 25 May 2026 10:26:17 |
| Eccentricity: | 0.0000872 |
| inclination: | 50.0099° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 167.3478° |
| argument of perigee: | 283.3958° |
| revolutions per day: | 13.29325295 |
| mean anomaly at epoch: | 76.6817° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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