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 36510U 10013C 25198.84272574 .00001709 00000-0 26368-3 0 9999
2 36510 92.0150 221.4176 0022611 114.1918 246.1668 14.73145530815239
| Epoch (UTC): | 17 July 2025 20:13:31 |
| Eccentricity: | 0.0022611 |
| inclination: | 92.0150° |
| perigee height: | 635 km |
| apogee height: | 667 km |
| right ascension of ascending node: | 221.4176° |
| argument of perigee: | 114.1918° |
| revolutions per day: | 14.73145530 |
| mean anomaly at epoch: | 246.1668° |
| orbit number at epoch: | 81523 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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