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 05118U 71028B 25188.58007132 .00014684 00000-0 29835-3 0 9996
2 05118 81.2419 350.6759 0024689 74.6987 285.6984 15.45843255950645
Epoch (UTC): | 07 July 2025 13:55:18 |
Eccentricity: | 0.0024689 |
inclination: | 81.2419° |
perigee height: | 412 km |
apogee height: | 446 km |
right ascension of ascending node: | 350.6759° |
argument of perigee: | 74.6987° |
revolutions per day: | 15.45843255 |
mean anomaly at epoch: | 285.6984° |
orbit number at epoch: | 95064 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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