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 23088U 94023B 24306.55295024 .00000566 00000-0 31749-3 0 9990
2 23088 71.0022 26.4439 0004910 304.9046 55.1614 14.14903252576330
Epoch (UTC): | 01 November 2024 13:16:14 |
Eccentricity: | 0.0004910 |
inclination: | 71.0022° |
perigee height: | 839 km |
apogee height: | 846 km |
right ascension of ascending node: | 26.4439° |
argument of perigee: | 304.9046° |
revolutions per day: | 14.14903252 |
mean anomaly at epoch: | 55.1614° |
orbit number at epoch: | 57633 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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