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 63755U 26145.50352646 +.00000000 +00000-0 +11927-2 0 00000
2 63755 42.9974 189.4775 0001092 235.4793 124.5971 15.70827204 04
| Epoch (UTC): | 25 May 2026 12:05:04 |
| Eccentricity: | 0.0001092 |
| inclination: | 42.9974° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 189.4775° |
| argument of perigee: | 235.4793° |
| revolutions per day: | 15.70827204 |
| mean anomaly at epoch: | 124.5971° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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