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 23343U 94074B 25198.40195814 .00000324 00000-0 50465-4 0 9999
2 23343 97.7376 233.4271 0005147 266.6494 203.3463 14.79069510652468
Epoch (UTC): | 17 July 2025 09:38:49 |
Eccentricity: | 0.0005147 |
inclination: | 97.7376° |
perigee height: | 628 km |
apogee height: | 636 km |
right ascension of ascending node: | 233.4271° |
argument of perigee: | 266.6494° |
revolutions per day: | 14.79069510 |
mean anomaly at epoch: | 203.3463° |
orbit number at epoch: | 65246 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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