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 63588U 26145.01779138 +.00000000 +00000-0 +53153-3 0 00007
2 63588 43.0038 250.6460 0003564 271.6830 88.3614 15.27597506 05
| Epoch (UTC): | 25 May 2026 00:25:37 |
| Eccentricity: | 0.0003564 |
| inclination: | 43.0038° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 250.6460° |
| argument of perigee: | 271.6830° |
| revolutions per day: | 15.27597506 |
| mean anomaly at epoch: | 88.3614° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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