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 62576U 26145.64629421 +.00000000 +00000-0 +82731-4 0 00006
2 62576 54.9777 10.8307 0013473 29.8223 330.3499 13.80604988 08
| Epoch (UTC): | 25 May 2026 15:30:39 |
| Eccentricity: | 0.0013473 |
| inclination: | 54.9777° |
| perigee height: | 952 km |
| apogee height: | 972 km |
| right ascension of ascending node: | 10.8307° |
| argument of perigee: | 29.8223° |
| revolutions per day: | 13.80604988 |
| mean anomaly at epoch: | 330.3499° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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