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 62511U 26145.52875808 +.00000000 +00000-0 +14983-2 0 00006
2 62511 43.0016 327.5421 0002395 268.2552 91.8041 15.70871893 06
| Epoch (UTC): | 25 May 2026 12:41:24 |
| Eccentricity: | 0.0002395 |
| inclination: | 43.0016° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 327.5421° |
| argument of perigee: | 268.2552° |
| revolutions per day: | 15.70871893 |
| mean anomaly at epoch: | 91.8041° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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