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 25198.88781685 .00000217 00000-0 39178-3 0 9994
2 14096 72.3009 349.8227 1093284 49.7312 319.4248 12.09944186860987
Epoch (UTC): | 17 July 2025 21:18:27 |
Eccentricity: | 0.1093284 |
inclination: | 72.3009° |
perigee height: | 760 km |
apogee height: | 2513 km |
right ascension of ascending node: | 349.8227° |
argument of perigee: | 49.7312° |
revolutions per day: | 12.09944186 |
mean anomaly at epoch: | 319.4248° |
orbit number at epoch: | 86098 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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