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 13553U 26138.09281784 +.00000000 +00000-0 +30113-4 0 00001
2 13553 82.5680 76.4586 0021920 72.3075 298.3559 14.86721967 04
| Epoch (UTC): | 18 May 2026 02:13:39 |
| Eccentricity: | 0.0021920 |
| inclination: | 82.5680° |
| perigee height: | 593 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 76.4586° |
| argument of perigee: | 72.3075° |
| revolutions per day: | 14.86721967 |
| mean anomaly at epoch: | 298.3559° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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