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 25636U 99008C 23274.18825519 .00000757 00000-0 19857-3 0 9997
2 25636 96.4865 8.5829 0143002 234.4656 124.3137 14.45271341296431
| Epoch (UTC): | 01 October 2023 04:31:05 |
| Eccentricity: | 0.0143002 |
| inclination: | 96.4865° |
| perigee height: | 639 km |
| apogee height: | 843 km |
| right ascension of ascending node: | 8.5829° |
| argument of perigee: | 234.4656° |
| revolutions per day: | 14.45271341 |
| mean anomaly at epoch: | 124.3137° |
| orbit number at epoch: | 29643 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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