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 23405U 94077B 25198.23964085 -.00000195 00000-0 -75248-4 0 9990
2 23405 70.9834 127.8161 0002883 213.7311 146.3628 14.15523566583185
Epoch (UTC): | 17 July 2025 05:45:04 |
Eccentricity: | 0.0002883 |
inclination: | 70.9834° |
perigee height: | 838 km |
apogee height: | 842 km |
right ascension of ascending node: | 127.8161° |
argument of perigee: | 213.7311° |
revolutions per day: | 14.15523566 |
mean anomaly at epoch: | 146.3628° |
orbit number at epoch: | 58318 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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