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 11U 59001A 24312.86435582 .00001848 00000-0 96045-3 0 9998
2 11 32.8700 142.0193 1454198 323.4439 27.4970 11.88893206807352
Epoch (UTC): | 07 November 2024 20:44:40 |
Eccentricity: | 0.1454198 |
inclination: | 32.8700° |
perigee height: | 552 km |
apogee height: | 2910 km |
right ascension of ascending node: | 142.0193° |
argument of perigee: | 323.4439° |
revolutions per day: | 11.88893206 |
mean anomaly at epoch: | 27.4970° |
orbit number at epoch: | 80735 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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