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 6061U 72043B 24279.16580362 .00001627 00000-0 50778-3 0 9990
2 6061 74.0540 292.6896 0018307 114.9848 245.3212 14.41530688742395
Epoch (UTC): | 05 October 2024 03:58:45 |
Eccentricity: | 0.0018307 |
inclination: | 74.0540° |
perigee height: | 740 km |
apogee height: | 766 km |
right ascension of ascending node: | 292.6896° |
argument of perigee: | 114.9848° |
revolutions per day: | 14.41530688 |
mean anomaly at epoch: | 245.3212° |
orbit number at epoch: | 74239 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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