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 25774U 99031E 23151.84908007 -.00000120 00000-0 16418-4 0 9993
2 25774 51.5275 289.6352 0374776 37.3627 122.6710 13.46540712179389
| Epoch (UTC): | 31 May 2023 20:22:40 |
| Eccentricity: | 0.0374776 |
| inclination: | 51.5275° |
| perigee height: | 805 km |
| apogee height: | 1365 km |
| right ascension of ascending node: | 289.6352° |
| argument of perigee: | 37.3627° |
| revolutions per day: | 13.46540712 |
| mean anomaly at epoch: | 122.6710° |
| orbit number at epoch: | 17938 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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