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 00053U 60009E 23336.95624446 -.00000051 00000-0 32851-3 0 9999
2 00053 47.2788 322.3727 0099640 216.2864 143.1138 12.17317605822476
Epoch (UTC): | 02 December 2023 22:56:59 |
Eccentricity: | 0.0099640 |
inclination: | 47.2788° |
perigee height: | 1525 km |
apogee height: | 1684 km |
right ascension of ascending node: | 322.3727° |
argument of perigee: | 216.2864° |
revolutions per day: | 12.17317605 |
mean anomaly at epoch: | 143.1138° |
orbit number at epoch: | 82247 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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