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 56100U 26145.24407807 +.00000000 +00000-0 +33922-4 0 00008
2 56100 43.0035 88.8841 0001503 282.6768 77.3916 15.27575990 07
| Epoch (UTC): | 25 May 2026 05:51:28 |
| Eccentricity: | 0.0001503 |
| inclination: | 43.0035° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 88.8841° |
| argument of perigee: | 282.6768° |
| revolutions per day: | 15.27575990 |
| mean anomaly at epoch: | 77.3916° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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