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 17590U 87027B 24276.78251507 .00000093 00000-0 70123-4 0 9991
2 17590 71.0024 298.2804 0006228 221.0833 138.9822 14.17022681941300
| Epoch (UTC): | 02 October 2024 18:46:49 |
| Eccentricity: | 0.0006228 |
| inclination: | 71.0024° |
| perigee height: | 831 km |
| apogee height: | 840 km |
| right ascension of ascending node: | 298.2804° |
| argument of perigee: | 221.0833° |
| revolutions per day: | 14.17022681 |
| mean anomaly at epoch: | 138.9822° |
| orbit number at epoch: | 94130 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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