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 57784U 26145.35159785 +.00000000 +00000-0 +86850-4 0 00006
2 57784 43.0015 121.3354 0001294 267.3492 92.7211 15.27569909 09
| Epoch (UTC): | 25 May 2026 08:26:18 |
| Eccentricity: | 0.0001294 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 121.3354° |
| argument of perigee: | 267.3492° |
| revolutions per day: | 15.27569909 |
| mean anomaly at epoch: | 92.7211° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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