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 12785U 81082A 24259.06369582 .00027187 00000-0 74780-3 0 9997
2 12785 82.4970 322.4219 0000876 110.1826 249.9512 15.37047947353941
Epoch (UTC): | 15 September 2024 01:31:43 |
Eccentricity: | 0.0000876 |
inclination: | 82.4970° |
perigee height: | 454 km |
apogee height: | 455 km |
right ascension of ascending node: | 322.4219° |
argument of perigee: | 110.1826° |
revolutions per day: | 15.37047947 |
mean anomaly at epoch: | 249.9512° |
orbit number at epoch: | 35394 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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