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 05485U 71080A 23275.73158764 .00000020 00000-0 82850-6 0 9999
2 05485 32.0564 59.9457 0640284 343.7257 14.3622 12.74175253423125
Epoch (UTC): | 02 October 2023 17:33:29 |
Eccentricity: | 0.0640284 |
inclination: | 32.0564° |
perigee height: | 869 km |
apogee height: | 1861 km |
right ascension of ascending node: | 59.9457° |
argument of perigee: | 343.7257° |
revolutions per day: | 12.74175253 |
mean anomaly at epoch: | 14.3622° |
orbit number at epoch: | 42312 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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