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 63556U 26145.43059308 +.00000000 +00000-0 +14885-2 0 00006
2 63556 43.0029 51.6155 0000785 281.6193 78.4587 15.70886206 00
| Epoch (UTC): | 25 May 2026 10:20:03 |
| Eccentricity: | 0.0000785 |
| inclination: | 43.0029° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 51.6155° |
| argument of perigee: | 281.6193° |
| revolutions per day: | 15.70886206 |
| mean anomaly at epoch: | 78.4587° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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