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 67632U 26145.47126821 +.00000000 +00000-0 +79675-3 0 00003
2 67632 43.0012 66.3855 0000946 259.4202 100.6543 15.27594075 06
| Epoch (UTC): | 25 May 2026 11:18:37 |
| Eccentricity: | 0.0000946 |
| inclination: | 43.0012° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 66.3855° |
| argument of perigee: | 259.4202° |
| revolutions per day: | 15.27594075 |
| mean anomaly at epoch: | 100.6543° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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