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 37966U 93036BPR 24354.36734572 .00025005 00000-0 30138-2 0 9996
2 37966 73.9867 237.9040 0019117 184.8094 175.2904 14.83623968799802
Epoch (UTC): | 19 December 2024 08:48:58 |
Eccentricity: | 0.0019117 |
inclination: | 73.9867° |
perigee height: | 604 km |
apogee height: | 631 km |
right ascension of ascending node: | 237.9040° |
argument of perigee: | 184.8094° |
revolutions per day: | 14.83623968 |
mean anomaly at epoch: | 175.2904° |
orbit number at epoch: | 79980 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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