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 23751U 26073.61819544 +.00000000 +00000-0 +78153-4 0 00005
2 23751 99.0287 90.2569 0000878 94.9814 265.1463 14.23543782 00
| Epoch (UTC): | 14 March 2026 14:50:12 |
| Eccentricity: | 0.0000878 |
| inclination: | 99.0287° |
| perigee height: | 813 km |
| apogee height: | 814 km |
| right ascension of ascending node: | 90.2569° |
| argument of perigee: | 94.9814° |
| revolutions per day: | 14.23543782 |
| mean anomaly at epoch: | 265.1463° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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