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 63585U 26145.63825237 +.00000000 +00000-0 +62713-3 0 00006
2 63585 42.9993 246.6976 0001525 276.5641 83.5037 15.27597495 09
| Epoch (UTC): | 25 May 2026 15:19:05 |
| Eccentricity: | 0.0001525 |
| inclination: | 42.9993° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 246.6976° |
| argument of perigee: | 276.5641° |
| revolutions per day: | 15.27597495 |
| mean anomaly at epoch: | 83.5037° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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