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 34823U 93036ABN 23333.33735871 .00003613 00000-0 81139-3 0 9990
2 34823 74.0458 63.8753 0172954 335.2635 24.0299 14.48042392775807
Epoch (UTC): | 29 November 2023 08:05:47 |
Eccentricity: | 0.0172954 |
inclination: | 74.0458° |
perigee height: | 609 km |
apogee height: | 855 km |
right ascension of ascending node: | 63.8753° |
argument of perigee: | 335.2635° |
revolutions per day: | 14.48042392 |
mean anomaly at epoch: | 24.0299° |
orbit number at epoch: | 77580 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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