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 24277.18663336 .00014762 00000-0 16100-2 0 9996
2 40057 98.3259 137.6319 0009361 142.9647 217.2216 14.88024756553757
| Epoch (UTC): | 03 October 2024 04:28:45 |
| Eccentricity: | 0.0009361 |
| inclination: | 98.3259° |
| perigee height: | 597 km |
| apogee height: | 610 km |
| right ascension of ascending node: | 137.6319° |
| argument of perigee: | 142.9647° |
| revolutions per day: | 14.88024756 |
| mean anomaly at epoch: | 217.2216° |
| orbit number at epoch: | 55375 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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