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 25188.60540044 .00001237 00000-0 10919-3 0 9994
2 23317 82.5329 223.7606 0016601 359.1284 0.9906 14.95468820663803
Epoch (UTC): | 07 July 2025 14:31:46 |
Eccentricity: | 0.0016601 |
inclination: | 82.5329° |
perigee height: | 569 km |
apogee height: | 592 km |
right ascension of ascending node: | 223.7606° |
argument of perigee: | 359.1284° |
revolutions per day: | 14.95468820 |
mean anomaly at epoch: | 0.9906° |
orbit number at epoch: | 66380 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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