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 42829U 17042E 25139.05412466 .00003685 00000-0 28796-3 0 9994
2 42829 97.3935 308.7963 0013679 359.0177 1.1019 15.01603747427499
Epoch (UTC): | 19 May 2025 01:17:56 |
Eccentricity: | 0.0013679 |
inclination: | 97.3935° |
perigee height: | 552 km |
apogee height: | 571 km |
right ascension of ascending node: | 308.7963° |
argument of perigee: | 359.0177° |
revolutions per day: | 15.01603747 |
mean anomaly at epoch: | 1.1019° |
orbit number at epoch: | 42749 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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