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 56333U 26145.44546306 +.00000000 +00000-0 -13856-4 0 00001
2 56333 97.4458 146.4615 0001593 77.6353 282.5053 15.05645233 04
| Epoch (UTC): | 25 May 2026 10:41:28 |
| Eccentricity: | 0.0001593 |
| inclination: | 97.4458° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 146.4615° |
| argument of perigee: | 77.6353° |
| revolutions per day: | 15.05645233 |
| mean anomaly at epoch: | 282.5053° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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