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 62124U 26145.08191255 +.00000000 +00000-0 +63047-3 0 00000
2 62124 43.0010 64.6363 0000984 273.4636 86.6104 15.27591695 00
| Epoch (UTC): | 25 May 2026 01:57:57 |
| Eccentricity: | 0.0000984 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 64.6363° |
| argument of perigee: | 273.4636° |
| revolutions per day: | 15.27591695 |
| mean anomaly at epoch: | 86.6104° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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