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 is defined by the following mean orbital elements,
1 14781U 26074.17847501 +.00000000 +00000-0 +19671-3 0 00003
2 14781 97.7955 40.8755 0008762 127.6246 232.5769 14.90527996 01
| Epoch (UTC): | 15 March 2026 04:17:00 |
| Eccentricity: | 0.0008762 |
| inclination: | 97.7955° |
| perigee height: | 590 km |
| apogee height: | 602 km |
| right ascension of ascending node: | 40.8755° |
| argument of perigee: | 127.6246° |
| revolutions per day: | 14.90527996 |
| mean anomaly at epoch: | 232.5769° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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