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 25199.51167635 .00001415 00000-0 12521-3 0 9996
2 23317 82.5325 213.3692 0015601 321.0819 38.9278 14.95497811665436
Epoch (UTC): | 18 July 2025 12:16:48 |
Eccentricity: | 0.0015601 |
inclination: | 82.5325° |
perigee height: | 570 km |
apogee height: | 591 km |
right ascension of ascending node: | 213.3692° |
argument of perigee: | 321.0819° |
revolutions per day: | 14.95497811 |
mean anomaly at epoch: | 38.9278° |
orbit number at epoch: | 66543 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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