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 21809U 91076E 25139.51763705 .00004002 00000-0 35987-3 0 9998
2 21809 63.2986 126.0136 0900239 67.2077 302.1466 13.53067875 50931
Epoch (UTC): | 19 May 2025 12:25:23 |
Eccentricity: | 0.0900239 |
inclination: | 63.2986° |
perigee height: | 391 km |
apogee height: | 1730 km |
right ascension of ascending node: | 126.0136° |
argument of perigee: | 67.2077° |
revolutions per day: | 13.53067875 |
mean anomaly at epoch: | 302.1466° |
orbit number at epoch: | 5093 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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