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 40057U 14034E 24261.11321304 .00011036 00000-0 12164-2 0 9995
2 40057 98.3295 120.7608 0008154 194.8543 165.2433 14.87678980551362
| Epoch (UTC): | 17 September 2024 02:43:01 |
| Eccentricity: | 0.0008154 |
| inclination: | 98.3295° |
| perigee height: | 599 km |
| apogee height: | 611 km |
| right ascension of ascending node: | 120.7608° |
| argument of perigee: | 194.8543° |
| revolutions per day: | 14.87678980 |
| mean anomaly at epoch: | 165.2433° |
| orbit number at epoch: | 55136 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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