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 57515U 26145.48401161 +.00000000 +00000-0 -11809-4 0 00003
2 57515 43.0031 302.0651 0001122 275.4371 84.6353 15.27580279 03
| Epoch (UTC): | 25 May 2026 11:36:58 |
| Eccentricity: | 0.0001122 |
| inclination: | 43.0031° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 302.0651° |
| argument of perigee: | 275.4371° |
| revolutions per day: | 15.27580279 |
| mean anomaly at epoch: | 84.6353° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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