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 67965U 26145.01571936 +.00000000 +00000-0 +24859-3 0 00007
2 67965 97.2836 155.0039 0001940 113.0255 247.1193 15.33454470 07
| Epoch (UTC): | 25 May 2026 00:22:38 |
| Eccentricity: | 0.0001940 |
| inclination: | 97.2836° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 155.0039° |
| argument of perigee: | 113.0255° |
| revolutions per day: | 15.33454470 |
| mean anomaly at epoch: | 247.1193° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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