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 25198.84959803 .00000002 00000-0 -13774-4 0 9992
2 21153 82.9262 165.8570 0028939 178.3526 216.2876 13.76288071724466
| Epoch (UTC): | 17 July 2025 20:23:25 |
| Eccentricity: | 0.0028939 |
| inclination: | 82.9262° |
| perigee height: | 956 km |
| apogee height: | 998 km |
| right ascension of ascending node: | 165.8570° |
| argument of perigee: | 178.3526° |
| revolutions per day: | 13.76288071 |
| mean anomaly at epoch: | 216.2876° |
| orbit number at epoch: | 72446 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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