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 30167U 99025TY 25134.13364257 .00001846 00000-0 45045-3 0 9998
2 30167 98.9792 206.1966 0146447 71.2658 309.4040 14.47672468962947
Epoch (UTC): | 14 May 2025 03:12:26 |
Eccentricity: | 0.0146447 |
inclination: | 98.9792° |
perigee height: | 629 km |
apogee height: | 837 km |
right ascension of ascending node: | 206.1966° |
argument of perigee: | 71.2658° |
revolutions per day: | 14.47672468 |
mean anomaly at epoch: | 309.4040° |
orbit number at epoch: | 96294 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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