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 57923U 26144.99687983 +.00000000 +00000-0 +21708-4 0 00007
2 57923 43.0010 254.6507 0001182 275.9665 84.1052 15.27577360 00
| Epoch (UTC): | 24 May 2026 23:55:30 |
| Eccentricity: | 0.0001182 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 254.6507° |
| argument of perigee: | 275.9665° |
| revolutions per day: | 15.27577360 |
| mean anomaly at epoch: | 84.1052° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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