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 36048U 93036AXK 24256.87434517 .00004626 00000-0 15766-2 0 9995
2 36048 74.0571 56.9160 0027455 224.7414 286.9315 14.36529464789520
Epoch (UTC): | 12 September 2024 20:59:03 |
Eccentricity: | 0.0027455 |
inclination: | 74.0571° |
perigee height: | 750 km |
apogee height: | 789 km |
right ascension of ascending node: | 56.9160° |
argument of perigee: | 224.7414° |
revolutions per day: | 14.36529464 |
mean anomaly at epoch: | 286.9315° |
orbit number at epoch: | 78952 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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