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 28230U 04014A 23266.52855127 .00001571 00000-0 20598-3 0 9999
2 28230 89.8171 71.0248 0001699 92.2843 267.8575 14.79958331504612
Epoch (UTC): | 23 September 2023 12:41:06 |
Eccentricity: | 0.0001699 |
inclination: | 89.8171° |
perigee height: | 628 km |
apogee height: | 630 km |
right ascension of ascending node: | 71.0248° |
argument of perigee: | 92.2843° |
revolutions per day: | 14.79958331 |
mean anomaly at epoch: | 267.8575° |
orbit number at epoch: | 50461 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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