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 21153U 91019B 25193.71584105 -.00000017 00000-0 -32615-4 0 9994
2 21153 82.9256 169.6763 0028594 192.8343 340.2504 13.76288168723754
| Epoch (UTC): | 12 July 2025 17:10:48 |
| Eccentricity: | 0.0028594 |
| inclination: | 82.9256° |
| perigee height: | 956 km |
| apogee height: | 998 km |
| right ascension of ascending node: | 169.6763° |
| argument of perigee: | 192.8343° |
| revolutions per day: | 13.76288168 |
| mean anomaly at epoch: | 340.2504° |
| orbit number at epoch: | 72375 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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