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 67106U 26145.21627420 +.00000000 +00000-0 +57647-3 0 00007
2 67106 42.9993 96.4955 0001060 266.2729 93.8001 15.27602320 06
| Epoch (UTC): | 25 May 2026 05:11:26 |
| Eccentricity: | 0.0001060 |
| inclination: | 42.9993° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 96.4955° |
| argument of perigee: | 266.2729° |
| revolutions per day: | 15.27602320 |
| mean anomaly at epoch: | 93.8001° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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