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 00012U 59001B 23341.11677421 .00000439 00000-0 23487-3 0 9993
2 00012 32.9101 232.2536 1660384 265.8647 75.1327 11.45891338425278
Epoch (UTC): | 07 December 2023 02:48:09 |
Eccentricity: | 0.1660384 |
inclination: | 32.9101° |
perigee height: | 553 km |
apogee height: | 3312 km |
right ascension of ascending node: | 232.2536° |
argument of perigee: | 265.8647° |
revolutions per day: | 11.45891338 |
mean anomaly at epoch: | 75.1327° |
orbit number at epoch: | 42527 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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