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 31133U 07012R 24336.85304955 .00005091 00000-0 94085-3 0 9992
2 31133 98.3692 297.9819 0073078 283.4596 75.8470 14.64152050937993
Epoch (UTC): | 01 December 2024 20:28:23 |
Eccentricity: | 0.0073078 |
inclination: | 98.3692° |
perigee height: | 628 km |
apogee height: | 731 km |
right ascension of ascending node: | 297.9819° |
argument of perigee: | 283.4596° |
revolutions per day: | 14.64152050 |
mean anomaly at epoch: | 75.8470° |
orbit number at epoch: | 93799 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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