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 25861U 99039B 23156.69229862 .00000564 00000-0 82974-4 0 9992
2 25861 98.1386 193.8669 0014004 276.8601 83.1016 14.79333998287710
Epoch (UTC): | 05 June 2023 16:36:54 |
Eccentricity: | 0.0014004 |
inclination: | 98.1386° |
perigee height: | 621 km |
apogee height: | 641 km |
right ascension of ascending node: | 193.8669° |
argument of perigee: | 276.8601° |
revolutions per day: | 14.79333998 |
mean anomaly at epoch: | 83.1016° |
orbit number at epoch: | 28771 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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