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 25192.48896911 .00000060 00000-0 26351-4 0 9996
2 10521 74.0247 211.0844 0021357 228.4960 131.4364 14.42192401496340
| Epoch (UTC): | 11 July 2025 11:44:06 |
| Eccentricity: | 0.0021357 |
| inclination: | 74.0247° |
| perigee height: | 736 km |
| apogee height: | 766 km |
| right ascension of ascending node: | 211.0844° |
| argument of perigee: | 228.4960° |
| revolutions per day: | 14.42192401 |
| mean anomaly at epoch: | 131.4364° |
| orbit number at epoch: | 49634 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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