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 63403U 26145.40093034 +.00000000 +00000-0 +74474-3 0 00009
2 63403 43.0000 33.7057 0000469 326.1204 33.9618 15.27585549 08
| Epoch (UTC): | 25 May 2026 09:37:20 |
| Eccentricity: | 0.0000469 |
| inclination: | 43.0000° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 33.7057° |
| argument of perigee: | 326.1204° |
| revolutions per day: | 15.27585549 |
| mean anomaly at epoch: | 33.9618° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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