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 63151U 26145.16604782 +.00000000 +00000-0 +29419-3 0 00009
2 63151 43.0028 303.8783 0001488 257.3569 102.7117 15.27574744 00
| Epoch (UTC): | 25 May 2026 03:59:06 |
| Eccentricity: | 0.0001488 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 303.8783° |
| argument of perigee: | 257.3569° |
| revolutions per day: | 15.27574744 |
| mean anomaly at epoch: | 102.7117° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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