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 20580U 90037B 25342.28548427 .00010003 00000-0 34811-3 0 9994
2 20580 28.4697 302.8053 0001895 185.8337 174.2236 15.27955239759310
| Epoch (UTC): | 08 December 2025 06:51:05 |
| Eccentricity: | 0.0001895 |
| inclination: | 28.4697° |
| perigee height: | 480 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 302.8053° |
| argument of perigee: | 185.8337° |
| revolutions per day: | 15.27955239 |
| mean anomaly at epoch: | 174.2236° |
| orbit number at epoch: | 75931 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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