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 56958U 26145.46676615 +.00000000 +00000-0 +33684-3 0 00002
2 56958 97.6185 292.8384 0006359 26.2508 333.9062 15.47037390 08
| Epoch (UTC): | 25 May 2026 11:12:08 |
| Eccentricity: | 0.0006359 |
| inclination: | 97.6185° |
| perigee height: | 421 km |
| apogee height: | 430 km |
| right ascension of ascending node: | 292.8384° |
| argument of perigee: | 26.2508° |
| revolutions per day: | 15.47037390 |
| mean anomaly at epoch: | 333.9062° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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