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 25188.63686326 -.00000198 00000-0 -30226-3 0 9997
2 14096 72.3004 4.1150 1093018 62.4044 308.3658 12.09943952859538
Epoch (UTC): | 07 July 2025 15:17:04 |
Eccentricity: | 0.1093018 |
inclination: | 72.3004° |
perigee height: | 760 km |
apogee height: | 2512 km |
right ascension of ascending node: | 4.1150° |
argument of perigee: | 62.4044° |
revolutions per day: | 12.09943952 |
mean anomaly at epoch: | 308.3658° |
orbit number at epoch: | 85953 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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