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 25509U 26154.76352465 +.00000000 +00000-0 +11686-3 0 00005
2 25509 31.4303 191.2056 0336384 315.9241 41.5024 14.33370182 01
| Epoch (UTC): | 03 June 2026 18:19:28 |
| Eccentricity: | 0.0336384 |
| inclination: | 31.4303° |
| perigee height: | 540 km |
| apogee height: | 1021 km |
| right ascension of ascending node: | 191.2056° |
| argument of perigee: | 315.9241° |
| revolutions per day: | 14.33370182 |
| mean anomaly at epoch: | 41.5024° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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