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 14096U 83051B 23156.51864504 -.00000534 00000-0 -84536-3 0 9990
2 14096 72.3030 347.9259 1094987 285.0582 63.1985 12.09784843767439
Epoch (UTC): | 05 June 2023 12:26:50 |
Eccentricity: | 0.1094987 |
inclination: | 72.3030° |
perigee height: | 759 km |
apogee height: | 2515 km |
right ascension of ascending node: | 347.9259° |
argument of perigee: | 285.0582° |
revolutions per day: | 12.09784843 |
mean anomaly at epoch: | 63.1985° |
orbit number at epoch: | 76743 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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