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 16720U 86034B 25198.50359503 .00000358 00000-0 38637-4 0 9999
2 16720 82.5534 7.0652 0020879 76.0967 337.8627 14.85370813 95950
Epoch (UTC): | 17 July 2025 12:05:10 |
Eccentricity: | 0.0020879 |
inclination: | 82.5534° |
perigee height: | 598 km |
apogee height: | 627 km |
right ascension of ascending node: | 7.0652° |
argument of perigee: | 76.0967° |
revolutions per day: | 14.85370813 |
mean anomaly at epoch: | 337.8627° |
orbit number at epoch: | 9595 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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