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 23147.20457699 .00000465 00000-0 52423-4 0 9995
2 15370 82.5140 132.7464 0022397 96.2583 264.1185 14.84261391 85954
| Epoch (UTC): | 27 May 2023 04:54:35 |
| Eccentricity: | 0.0022397 |
| inclination: | 82.5140° |
| perigee height: | 600 km |
| apogee height: | 631 km |
| right ascension of ascending node: | 132.7464° |
| argument of perigee: | 96.2583° |
| revolutions per day: | 14.84261391 |
| mean anomaly at epoch: | 264.1185° |
| orbit number at epoch: | 8595 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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