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 39211U 13037D 25196.96112212 .00008095 00000-0 26685-3 0 9999
2 39211 97.9791 89.6183 0079943 21.0117 339.4374 15.28657128659366
Epoch (UTC): | 15 July 2025 23:04:00 |
Eccentricity: | 0.0079943 |
inclination: | 97.9791° |
perigee height: | 425 km |
apogee height: | 534 km |
right ascension of ascending node: | 89.6183° |
argument of perigee: | 21.0117° |
revolutions per day: | 15.28657128 |
mean anomaly at epoch: | 339.4374° |
orbit number at epoch: | 65936 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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