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 31012U 99025BDE 23339.19941269 .00000647 00000-0 27714-3 0 9994
2 31012 98.9973 208.8769 0083001 228.9124 259.1376 14.26622899872126
Epoch (UTC): | 05 December 2023 04:47:09 |
Eccentricity: | 0.0083001 |
inclination: | 98.9973° |
perigee height: | 743 km |
apogee height: | 862 km |
right ascension of ascending node: | 208.8769° |
argument of perigee: | 228.9124° |
revolutions per day: | 14.26622899 |
mean anomaly at epoch: | 259.1376° |
orbit number at epoch: | 87212 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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