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 23265.81195482 .00005112 00000-0 64019-3 0 9996
2 40057 98.3680 103.3051 0008714 292.1063 67.9223 14.82700161497894
| Epoch (UTC): | 22 September 2023 19:29:12 |
| Eccentricity: | 0.0008714 |
| inclination: | 98.3680° |
| perigee height: | 615 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 103.3051° |
| argument of perigee: | 292.1063° |
| revolutions per day: | 14.82700161 |
| mean anomaly at epoch: | 67.9223° |
| orbit number at epoch: | 49789 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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