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 59131U 26145.65966398 +.00000000 +00000-0 +17679-3 0 00005
2 59131 97.5611 283.3789 0009141 327.5241 32.5436 15.30854707 02
| Epoch (UTC): | 25 May 2026 15:49:54 |
| Eccentricity: | 0.0009141 |
| inclination: | 97.5611° |
| perigee height: | 467 km |
| apogee height: | 480 km |
| right ascension of ascending node: | 283.3789° |
| argument of perigee: | 327.5241° |
| revolutions per day: | 15.30854707 |
| mean anomaly at epoch: | 32.5436° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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