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 57925U 26144.67252183 +.00000000 +00000-0 -22034-4 0 00008
2 57925 43.0029 256.5169 0001481 270.9315 89.1367 15.27571239 09
| Epoch (UTC): | 24 May 2026 16:08:25 |
| Eccentricity: | 0.0001481 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 256.5169° |
| argument of perigee: | 270.9315° |
| revolutions per day: | 15.27571239 |
| mean anomaly at epoch: | 89.1367° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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