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 85U 61004C 24307.40749233 .00151262 00000-0 14977-1 0 9998
2 85 38.7202 331.1557 0211526 219.7462 138.7634 14.75283840160618
Epoch (UTC): | 02 November 2024 09:46:47 |
Eccentricity: | 0.0211526 |
inclination: | 38.7202° |
perigee height: | 496 km |
apogee height: | 793 km |
right ascension of ascending node: | 331.1557° |
argument of perigee: | 219.7462° |
revolutions per day: | 14.75283840 |
mean anomaly at epoch: | 138.7634° |
orbit number at epoch: | 16061 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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