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 63074U 26145.20361918 +.00000000 +00000-0 +66616-3 0 00009
2 63074 43.0026 74.7794 0001497 240.5180 119.5522 15.27580572 03
| Epoch (UTC): | 25 May 2026 04:53:12 |
| Eccentricity: | 0.0001497 |
| inclination: | 43.0026° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 74.7794° |
| argument of perigee: | 240.5180° |
| revolutions per day: | 15.27580572 |
| mean anomaly at epoch: | 119.5522° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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