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 26073.30576145 +.00000000 +00000-0 +19403-3 0 00003
2 14781 97.7953 40.0142 0008703 130.1245 230.0737 14.90524636 00
| Epoch (UTC): | 14 March 2026 07:20:17 |
| Eccentricity: | 0.0008703 |
| inclination: | 97.7953° |
| perigee height: | 590 km |
| apogee height: | 602 km |
| right ascension of ascending node: | 40.0142° |
| argument of perigee: | 130.1245° |
| revolutions per day: | 14.90524636 |
| mean anomaly at epoch: | 230.0737° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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