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 57878U 26145.53255187 +.00000000 +00000-0 -89660-4 0 00006
2 57878 43.0000 210.8834 0001264 269.3812 90.6895 15.27556994 04
| Epoch (UTC): | 25 May 2026 12:46:52 |
| Eccentricity: | 0.0001264 |
| inclination: | 43.0000° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 210.8834° |
| argument of perigee: | 269.3812° |
| revolutions per day: | 15.27556994 |
| mean anomaly at epoch: | 90.6895° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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