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 21088U 91006B 25198.49770855 .00000115 00000-0 10050-3 0 9991
2 21088 82.9441 345.0035 0021847 337.2584 85.3758 13.77464549731695
Epoch (UTC): | 17 July 2025 11:56:42 |
Eccentricity: | 0.0021847 |
inclination: | 82.9441° |
perigee height: | 957 km |
apogee height: | 989 km |
right ascension of ascending node: | 345.0035° |
argument of perigee: | 337.2584° |
revolutions per day: | 13.77464549 |
mean anomaly at epoch: | 85.3758° |
orbit number at epoch: | 73169 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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