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 56358U 26144.95952937 +.00000000 +00000-0 -14211-2 0 00008
2 56358 97.4532 144.9777 0001440 19.0292 341.0989 15.05728135 01
| Epoch (UTC): | 24 May 2026 23:01:43 |
| Eccentricity: | 0.0001440 |
| inclination: | 97.4532° |
| perigee height: | 548 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 144.9777° |
| argument of perigee: | 19.0292° |
| revolutions per day: | 15.05728135 |
| mean anomaly at epoch: | 341.0989° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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