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 63554U 26145.16032775 +.00000000 +00000-0 +15174-2 0 00005
2 63554 43.0018 53.0256 0001979 253.0368 107.0283 15.70903028 01
| Epoch (UTC): | 25 May 2026 03:50:52 |
| Eccentricity: | 0.0001979 |
| inclination: | 43.0018° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 53.0256° |
| argument of perigee: | 253.0368° |
| revolutions per day: | 15.70903028 |
| mean anomaly at epoch: | 107.0283° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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