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 37165U 10047A 23154.42261178 .00001449 00000-0 20802-3 0 9993
2 37165 98.4022 310.9505 0037580 191.4658 168.5699 14.77708610683944
| Epoch (UTC): | 03 June 2023 10:08:33 |
| Eccentricity: | 0.0037580 |
| inclination: | 98.4022° |
| perigee height: | 610 km |
| apogee height: | 663 km |
| right ascension of ascending node: | 310.9505° |
| argument of perigee: | 191.4658° |
| revolutions per day: | 14.77708610 |
| mean anomaly at epoch: | 168.5699° |
| orbit number at epoch: | 68394 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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