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 39763U 14028C 23088.21507112 .00000047 00000-0 26765-3 0 9993
2 39763 82.4448 125.5286 0022138 114.9051 245.4331 12.42917118401504
Epoch (UTC): | 29 March 2023 05:09:42 |
Eccentricity: | 0.0022138 |
inclination: | 82.4448° |
perigee height: | 1477 km |
apogee height: | 1511 km |
right ascension of ascending node: | 125.5286° |
argument of perigee: | 114.9051° |
revolutions per day: | 12.42917118 |
mean anomaly at epoch: | 245.4331° |
orbit number at epoch: | 40150 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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