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 20763U 90074B 25189.51578911 .00002021 00000-0 14718-3 0 9999
2 20763 24.7598 319.2377 0340802 21.8743 339.5949 14.60550410827206
| Epoch (UTC): | 08 July 2025 12:22:44 |
| Eccentricity: | 0.0340802 |
| inclination: | 24.7598° |
| perigee height: | 450 km |
| apogee height: | 932 km |
| right ascension of ascending node: | 319.2377° |
| argument of perigee: | 21.8743° |
| revolutions per day: | 14.60550410 |
| mean anomaly at epoch: | 339.5949° |
| orbit number at epoch: | 82720 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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