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 63524U 26145.75284703 +.00000000 +00000-0 +00000-0 0 00007
2 63524 1.0082 82.8583 0002816 292.0576 303.9397 1.00271713 01
| Epoch (UTC): | 25 May 2026 18:04:05 |
| Eccentricity: | 0.0002816 |
| inclination: | 1.0082° |
| perigee height: | 35775 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 82.8583° |
| argument of perigee: | 292.0576° |
| revolutions per day: | 1.00271713 |
| mean anomaly at epoch: | 303.9397° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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