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 10521U 77119B 25140.53277614 .00000322 00000-0 10580-3 0 9995
2 10521 74.0261 307.4810 0020845 332.6736 27.3322 14.42166006488855
| Epoch (UTC): | 20 May 2025 12:47:11 |
| Eccentricity: | 0.0020845 |
| inclination: | 74.0261° |
| perigee height: | 736 km |
| apogee height: | 766 km |
| right ascension of ascending node: | 307.4810° |
| argument of perigee: | 332.6736° |
| revolutions per day: | 14.42166006 |
| mean anomaly at epoch: | 27.3322° |
| orbit number at epoch: | 48885 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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