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 14781U 84021B 25118.87860111 .00002722 00000-0 29321-3 0 9998
2 14781 97.7512 86.0854 0009388 110.0458 250.1771 14.89243006195434
| Epoch (UTC): | 28 April 2025 21:05:11 |
| Eccentricity: | 0.0009388 |
| inclination: | 97.7512° |
| perigee height: | 594 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 86.0854° |
| argument of perigee: | 110.0458° |
| revolutions per day: | 14.89243006 |
| mean anomaly at epoch: | 250.1771° |
| orbit number at epoch: | 19543 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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