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 23710U 26150.00323501 +.00000000 +00000-0 +12642-3 0 00002
2 23710 98.5463 159.2307 0001605 92.8453 267.2915 14.32397910 01
| Epoch (UTC): | 30 May 2026 00:04:39 |
| Eccentricity: | 0.0001605 |
| inclination: | 98.5463° |
| perigee height: | 783 km |
| apogee height: | 785 km |
| right ascension of ascending node: | 159.2307° |
| argument of perigee: | 92.8453° |
| revolutions per day: | 14.32397910 |
| mean anomaly at epoch: | 267.2915° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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