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 67497U 26145.54696025 +.00000000 +00000-0 +48031-3 0 00000
2 67497 42.9991 240.5785 0001377 269.3882 90.6812 15.27595780 01
| Epoch (UTC): | 25 May 2026 13:07:37 |
| Eccentricity: | 0.0001377 |
| inclination: | 42.9991° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 240.5785° |
| argument of perigee: | 269.3882° |
| revolutions per day: | 15.27595780 |
| mean anomaly at epoch: | 90.6812° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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