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 44751U 26145.35360365 +.00000000 +00000-0 +97348-3 0 00007
2 44751 53.0479 203.8515 0007221 18.7938 341.3337 15.53329250 02
| Epoch (UTC): | 25 May 2026 08:29:11 |
| Eccentricity: | 0.0007221 |
| inclination: | 53.0479° |
| perigee height: | 402 km |
| apogee height: | 412 km |
| right ascension of ascending node: | 203.8515° |
| argument of perigee: | 18.7938° |
| revolutions per day: | 15.53329250 |
| mean anomaly at epoch: | 341.3337° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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