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 00085U 61004C 24311.33175496 .00136868 00000-0 13274-1 0 9993
2 00085 38.7188 309.2956 0208761 247.6553 110.1964 14.76466429161234
Epoch (UTC): | 06 November 2024 07:57:43 |
Eccentricity: | 0.0208761 |
inclination: | 38.7188° |
perigee height: | 494 km |
apogee height: | 787 km |
right ascension of ascending node: | 309.2956° |
argument of perigee: | 247.6553° |
revolutions per day: | 14.76466429 |
mean anomaly at epoch: | 110.1964° |
orbit number at epoch: | 16123 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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