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 26137.14385205 +.00000000 +00000-0 +66336-4 0 00009
2 14781 97.8040 103.0714 0006116 291.7324 68.3242 14.90703554 02
| Epoch (UTC): | 17 May 2026 03:27:08 |
| Eccentricity: | 0.0006116 |
| inclination: | 97.8040° |
| perigee height: | 591 km |
| apogee height: | 600 km |
| right ascension of ascending node: | 103.0714° |
| argument of perigee: | 291.7324° |
| revolutions per day: | 14.90703554 |
| mean anomaly at epoch: | 68.3242° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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