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 32953U 08025A 23157.50039885 .00000028 00000-0 13267-3 0 9995
2 32953 82.5019 323.7438 0019271 205.4287 154.5846 12.43124784682181
Epoch (UTC): | 06 June 2023 12:00:34 |
Eccentricity: | 0.0019271 |
inclination: | 82.5019° |
perigee height: | 1478 km |
apogee height: | 1508 km |
right ascension of ascending node: | 323.7438° |
argument of perigee: | 205.4287° |
revolutions per day: | 12.43124784 |
mean anomaly at epoch: | 154.5846° |
orbit number at epoch: | 68218 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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