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 15370U 84111B 23151.45172969 .00000511 00000-0 57871-4 0 9995
2 15370 82.5144 128.7604 0022392 83.2305 277.1457 14.84265749 65485
| Epoch (UTC): | 31 May 2023 10:50:29 |
| Eccentricity: | 0.0022392 |
| inclination: | 82.5144° |
| perigee height: | 600 km |
| apogee height: | 631 km |
| right ascension of ascending node: | 128.7604° |
| argument of perigee: | 83.2305° |
| revolutions per day: | 14.84265749 |
| mean anomaly at epoch: | 277.1457° |
| orbit number at epoch: | 6548 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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