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 26474U 26076.11724321 +.00000000 +00000-0 +22333-3 0 00004
2 26474 67.9910 19.6226 0038829 26.5531 333.7595 15.09638120 05
| Epoch (UTC): | 17 March 2026 02:48:49 |
| Eccentricity: | 0.0038829 |
| inclination: | 67.9910° |
| perigee height: | 510 km |
| apogee height: | 564 km |
| right ascension of ascending node: | 19.6226° |
| argument of perigee: | 26.5531° |
| revolutions per day: | 15.09638120 |
| mean anomaly at epoch: | 333.7595° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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