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 32791U 08021J 25114.16941979 .00018761 00000-0 94172-3 0 9991
2 32791 97.7250 93.2266 0003343 11.6205 348.5105 15.17351693923539
| Epoch (UTC): | 24 April 2025 04:03:57 |
| Eccentricity: | 0.0003343 |
| inclination: | 97.7250° |
| perigee height: | 511 km |
| apogee height: | 516 km |
| right ascension of ascending node: | 93.2266° |
| argument of perigee: | 11.6205° |
| revolutions per day: | 15.17351693 |
| mean anomaly at epoch: | 348.5105° |
| orbit number at epoch: | 92353 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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