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 46563U 26145.62218977 +.00000000 +00000-0 +11834-2 0 00006
2 46563 53.0252 112.8540 0005871 52.2936 307.8606 15.56468080 05
| Epoch (UTC): | 25 May 2026 14:55:57 |
| Eccentricity: | 0.0005871 |
| inclination: | 53.0252° |
| perigee height: | 394 km |
| apogee height: | 402 km |
| right ascension of ascending node: | 112.8540° |
| argument of perigee: | 52.2936° |
| revolutions per day: | 15.56468080 |
| mean anomaly at epoch: | 307.8606° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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