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 25544U 98067A 24252.52833367 .00030551 00000-0 56519-3 0 9995
2 25544 51.6387 262.5048 0007279 328.0279 135.9780 15.48740152471478
| Epoch (UTC): | 08 September 2024 12:40:48 |
| Eccentricity: | 0.0007279 |
| inclination: | 51.6387° |
| perigee height: | 415 km |
| apogee height: | 425 km |
| right ascension of ascending node: | 262.5048° |
| argument of perigee: | 328.0279° |
| revolutions per day: | 15.48740152 |
| mean anomaly at epoch: | 135.9780° |
| orbit number at epoch: | 47147 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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