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 24287.74738224 -.00000057 00000-0 -49113-5 0 9996
2 23088 70.9997 65.9278 0004460 321.9750 38.1057 14.14895882573674
Epoch (UTC): | 13 October 2024 17:56:13 |
Eccentricity: | 0.0004460 |
inclination: | 70.9997° |
perigee height: | 839 km |
apogee height: | 846 km |
right ascension of ascending node: | 65.9278° |
argument of perigee: | 321.9750° |
revolutions per day: | 14.14895882 |
mean anomaly at epoch: | 38.1057° |
orbit number at epoch: | 57367 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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