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 25073.19004423 .00026794 00000-0 14263-2 0 9999
2 32791 97.7222 51.5103 0007223 101.4643 258.7401 15.15183320917329
| Epoch (UTC): | 14 March 2025 04:33:39 |
| Eccentricity: | 0.0007223 |
| inclination: | 97.7222° |
| perigee height: | 515 km |
| apogee height: | 525 km |
| right ascension of ascending node: | 51.5103° |
| argument of perigee: | 101.4643° |
| revolutions per day: | 15.15183320 |
| mean anomaly at epoch: | 258.7401° |
| orbit number at epoch: | 91732 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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