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 44071U 19014A 24284.12879826 .00000052 00000-0 00000-0 0 9991
2 44071 0.0126 202.2593 0000172 276.2106 7.4728 1.00270736 20460
| Epoch (UTC): | 10 October 2024 03:05:28 |
| Eccentricity: | 0.0000172 |
| inclination: | 0.0126° |
| perigee height: | 35786 km |
| apogee height: | 35787 km |
| right ascension of ascending node: | 202.2593° |
| argument of perigee: | 276.2106° |
| revolutions per day: | 1.00270736 |
| mean anomaly at epoch: | 7.4728° |
| orbit number at epoch: | 2046 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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