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 data is extracted from the following two-line orbital elements,
1 20578U 90036B 25198.85145603 .00000041 00000-0 26310-4 0 9998
2 20578 82.9458 327.6421 0012899 6.7809 159.0821 13.76603656769870
| Epoch (UTC): | 17 July 2025 20:26:05 |
| Eccentricity: | 0.0012899 |
| inclination: | 82.9458° |
| perigee height: | 966 km |
| apogee height: | 985 km |
| right ascension of ascending node: | 327.6421° |
| argument of perigee: | 6.7809° |
| revolutions per day: | 13.76603656 |
| mean anomaly at epoch: | 159.0821° |
| orbit number at epoch: | 76987 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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