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 5118U 71028B 25194.14661378 .00016316 00000-0 32992-3 0 9995
2 5118 81.2434 343.9599 0024371 55.5852 304.7692 15.45993958951798
Epoch (UTC): | 13 July 2025 03:31:07 |
Eccentricity: | 0.0024371 |
inclination: | 81.2434° |
perigee height: | 412 km |
apogee height: | 445 km |
right ascension of ascending node: | 343.9599° |
argument of perigee: | 55.5852° |
revolutions per day: | 15.45993958 |
mean anomaly at epoch: | 304.7692° |
orbit number at epoch: | 95179 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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