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 37839U 11058B 24262.18100845 .00000894 00000-0 32925-3 0 9993
2 37839 19.9598 217.4077 0018583 242.4449 234.4303 14.13322237668787
Epoch (UTC): | 18 September 2024 04:20:39 |
Eccentricity: | 0.0018583 |
inclination: | 19.9598° |
perigee height: | 834 km |
apogee height: | 861 km |
right ascension of ascending node: | 217.4077° |
argument of perigee: | 242.4449° |
revolutions per day: | 14.13322237 |
mean anomaly at epoch: | 234.4303° |
orbit number at epoch: | 66878 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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