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 21263U 91032A 22148.91588459 .00000077 00000-0 50111-4 0 9991
2 21263 98.5134 149.2873 0014438 40.7120 319.5136 14.25991675613944
Epoch (UTC): | 28 May 2022 21:58:52 |
Eccentricity: | 0.0014438 |
inclination: | 98.5134° |
perigee height: | 795 km |
apogee height: | 815 km |
right ascension of ascending node: | 149.2873° |
argument of perigee: | 40.7120° |
revolutions per day: | 14.25991675 |
mean anomaly at epoch: | 319.5136° |
orbit number at epoch: | 61394 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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