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 12585U 81065A 23152.52628701 .00009188 00000-0 32403-3 0 9996
2 12585 97.5759 167.5285 0011522 0.2823 359.8422 15.29431354287417
Epoch (UTC): | 01 June 2023 12:37:51 |
Eccentricity: | 0.0011522 |
inclination: | 97.5759° |
perigee height: | 469 km |
apogee height: | 485 km |
right ascension of ascending node: | 167.5285° |
argument of perigee: | 0.2823° |
revolutions per day: | 15.29431354 |
mean anomaly at epoch: | 359.8422° |
orbit number at epoch: | 28741 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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