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 20562U 26087.91042713 +.00000000 +00000-0 +15523-3 0 00007
2 20562 89.8502 264.7374 0060854 228.2254 131.3759 14.76310689 04
| Epoch (UTC): | 28 March 2026 21:51:00 |
| Eccentricity: | 0.0060854 |
| inclination: | 89.8502° |
| perigee height: | 598 km |
| apogee height: | 684 km |
| right ascension of ascending node: | 264.7374° |
| argument of perigee: | 228.2254° |
| revolutions per day: | 14.76310689 |
| mean anomaly at epoch: | 131.3759° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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