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 39417U 13066B 25197.82185627 .00003635 00000-0 31617-3 0 9991
2 39417 97.7811 154.6477 0041991 288.2400 71.4253 14.96935610630488
Epoch (UTC): | 16 July 2025 19:43:28 |
Eccentricity: | 0.0041991 |
inclination: | 97.7811° |
perigee height: | 547 km |
apogee height: | 605 km |
right ascension of ascending node: | 154.6477° |
argument of perigee: | 288.2400° |
revolutions per day: | 14.96935610 |
mean anomaly at epoch: | 71.4253° |
orbit number at epoch: | 63048 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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