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 14699U 84013A 25198.73524557 .00005256 00000-0 24092-3 0 9996
2 14699 82.5483 340.6518 0016249 29.8788 330.3371 15.20122990258031
Epoch (UTC): | 17 July 2025 17:38:45 |
Eccentricity: | 0.0016249 |
inclination: | 82.5483° |
perigee height: | 494 km |
apogee height: | 516 km |
right ascension of ascending node: | 340.6518° |
argument of perigee: | 29.8788° |
revolutions per day: | 15.20122990 |
mean anomaly at epoch: | 330.3371° |
orbit number at epoch: | 25803 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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