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 26065.38411669 +.00000000 +00000-0 +27987-3 0 00007
2 14781 97.7948 32.1968 0008159 153.3011 206.8628 14.90492014 09
| Epoch (UTC): | 06 March 2026 09:13:07 |
| Eccentricity: | 0.0008159 |
| inclination: | 97.7948° |
| perigee height: | 591 km |
| apogee height: | 602 km |
| right ascension of ascending node: | 32.1968° |
| argument of perigee: | 153.3011° |
| revolutions per day: | 14.90492014 |
| mean anomaly at epoch: | 206.8628° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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