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 23317U 94066A 23088.81011134 .00003272 00000-0 34076-3 0 9998
2 23317 82.5346 291.0587 0017737 250.2556 109.6749 14.89438071539916
Epoch (UTC): | 29 March 2023 19:26:33 |
Eccentricity: | 0.0017737 |
inclination: | 82.5346° |
perigee height: | 587 km |
apogee height: | 612 km |
right ascension of ascending node: | 291.0587° |
argument of perigee: | 250.2556° |
revolutions per day: | 14.89438071 |
mean anomaly at epoch: | 109.6749° |
orbit number at epoch: | 53991 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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