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 57667U 26145.57987065 +.00000000 +00000-0 +15368-4 0 00006
2 57667 53.1588 209.9233 0001135 76.5262 283.5866 15.30192052 05
| Epoch (UTC): | 25 May 2026 13:55:00 |
| Eccentricity: | 0.0001135 |
| inclination: | 53.1588° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 209.9233° |
| argument of perigee: | 76.5262° |
| revolutions per day: | 15.30192052 |
| mean anomaly at epoch: | 283.5866° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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