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 32709U 08011B 25188.96824379 .00003021 00000-0 15971-1 0 9993
2 32709 49.1104 76.3666 6527601 156.7558 256.3191 3.08969393194539
| Epoch (UTC): | 07 July 2025 23:14:16 |
| Eccentricity: | 0.6527601 |
| inclination: | 49.1104° |
| perigee height: | 536 km |
| apogee height: | 26532 km |
| right ascension of ascending node: | 76.3666° |
| argument of perigee: | 156.7558° |
| revolutions per day: | 3.08969393 |
| mean anomaly at epoch: | 256.3191° |
| orbit number at epoch: | 19453 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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