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 67124U 26145.20471720 +.00000000 +00000-0 +63141-3 0 00002
2 67124 43.0004 96.4058 0001543 262.6580 97.4096 15.27587496 06
| Epoch (UTC): | 25 May 2026 04:54:47 |
| Eccentricity: | 0.0001543 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 96.4058° |
| argument of perigee: | 262.6580° |
| revolutions per day: | 15.27587496 |
| mean anomaly at epoch: | 97.4096° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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