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 00051U 60009C 24312.58303916 -.00000037 00000-0 45416-3 0 9992
2 00051 47.2139 64.4790 0107496 251.3095 107.6000 12.18342788859657
Epoch (UTC): | 07 November 2024 13:59:34 |
Eccentricity: | 0.0107496 |
inclination: | 47.2139° |
perigee height: | 1514 km |
apogee height: | 1685 km |
right ascension of ascending node: | 64.4790° |
argument of perigee: | 251.3095° |
revolutions per day: | 12.18342788 |
mean anomaly at epoch: | 107.6000° |
orbit number at epoch: | 85965 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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