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 26017.03708374 +.00000000 +00000-0 +56689-4 0 00007
2 23751 99.0300 32.2024 0001107 85.7800 274.3504 14.23520663 08
| Epoch (UTC): | 17 January 2026 00:53:24 |
| Eccentricity: | 0.0001107 |
| inclination: | 99.0300° |
| perigee height: | 813 km |
| apogee height: | 814 km |
| right ascension of ascending node: | 32.2024° |
| argument of perigee: | 85.7800° |
| revolutions per day: | 14.23520663 |
| mean anomaly at epoch: | 274.3504° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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