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 27422U 02021B 25133.79043401 .00000307 00000-0 13359-3 0 9998
2 27422 98.5602 71.5717 0011870 356.8651 3.2456 14.30774518201135
Epoch (UTC): | 13 May 2025 18:58:13 |
Eccentricity: | 0.0011870 |
inclination: | 98.5602° |
perigee height: | 780 km |
apogee height: | 797 km |
right ascension of ascending node: | 71.5717° |
argument of perigee: | 356.8651° |
revolutions per day: | 14.30774518 |
mean anomaly at epoch: | 3.2456° |
orbit number at epoch: | 20113 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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