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 63019U 26145.37373340 +.00000000 +00000-0 +83759-3 0 00005
2 63019 43.0013 263.3455 0001873 274.3576 85.7061 15.27581281 00
| Epoch (UTC): | 25 May 2026 08:58:10 |
| Eccentricity: | 0.0001873 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 263.3455° |
| argument of perigee: | 274.3576° |
| revolutions per day: | 15.27581281 |
| mean anomaly at epoch: | 85.7061° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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