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 34839U 09021A 25142.47190876 .00255549 29772-4 45478-3 0 9997
2 34839 97.1913 122.9866 0003002 75.3021 284.8592 16.01842258896532
Epoch (UTC): | 22 May 2025 11:19:32 |
Eccentricity: | 0.0003002 |
inclination: | 97.1913° |
perigee height: | 267 km |
apogee height: | 271 km |
right ascension of ascending node: | 122.9866° |
argument of perigee: | 75.3021° |
revolutions per day: | 16.01842258 |
mean anomaly at epoch: | 284.8592° |
orbit number at epoch: | 89653 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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