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 32955U 08025C 23088.49010426 .00000024 00000-0 10241-3 0 9993
2 32955 82.5077 4.4836 0021770 354.4825 5.6016 12.43328392673896
Epoch (UTC): | 29 March 2023 11:45:45 |
Eccentricity: | 0.0021770 |
inclination: | 82.5077° |
perigee height: | 1475 km |
apogee height: | 1509 km |
right ascension of ascending node: | 4.4836° |
argument of perigee: | 354.4825° |
revolutions per day: | 12.43328392 |
mean anomaly at epoch: | 5.6016° |
orbit number at epoch: | 67389 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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