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 57867U 26145.49026280 +.00000000 +00000-0 +73708-3 0 00003
2 57867 43.0031 211.4288 0001577 272.1471 87.9200 15.27588832 01
| Epoch (UTC): | 25 May 2026 11:45:58 |
| Eccentricity: | 0.0001577 |
| inclination: | 43.0031° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 211.4288° |
| argument of perigee: | 272.1471° |
| revolutions per day: | 15.27588832 |
| mean anomaly at epoch: | 87.9200° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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