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 30546U 99025AKL 24285.41440270 .00154625 00000-0 19665-1 0 9997
2 30546 98.9200 86.3307 0111884 75.8194 314.8439 14.76440494941348
| Epoch (UTC): | 11 October 2024 09:56:44 |
| Eccentricity: | 0.0111884 |
| inclination: | 98.9200° |
| perigee height: | 562 km |
| apogee height: | 719 km |
| right ascension of ascending node: | 86.3307° |
| argument of perigee: | 75.8194° |
| revolutions per day: | 14.76440494 |
| mean anomaly at epoch: | 314.8439° |
| orbit number at epoch: | 94134 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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