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 26042.05939439 +.00000000 +00000-0 +69745-4 0 00002
2 23751 99.0301 57.8751 0000979 83.0585 277.0704 14.23532576 04
| Epoch (UTC): | 11 February 2026 01:25:31 |
| Eccentricity: | 0.0000979 |
| inclination: | 99.0301° |
| perigee height: | 813 km |
| apogee height: | 814 km |
| right ascension of ascending node: | 57.8751° |
| argument of perigee: | 83.0585° |
| revolutions per day: | 14.23532576 |
| mean anomaly at epoch: | 277.0704° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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