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 31128U 07012M 23272.38044888 .00002452 00000-0 51173-3 0 9997
2 31128 98.3090 214.2726 0091856 285.8140 73.2946 14.58239882873501
Epoch (UTC): | 29 September 2023 09:07:50 |
Eccentricity: | 0.0091856 |
inclination: | 98.3090° |
perigee height: | 634 km |
apogee height: | 764 km |
right ascension of ascending node: | 214.2726° |
argument of perigee: | 285.8140° |
revolutions per day: | 14.58239882 |
mean anomaly at epoch: | 73.2946° |
orbit number at epoch: | 87350 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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