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 63552U 26144.74697806 +.00000000 +00000-0 +13362-2 0 00005
2 63552 43.0009 55.0689 0003610 281.3604 78.6858 15.70952013 01
| Epoch (UTC): | 24 May 2026 17:55:38 |
| Eccentricity: | 0.0003610 |
| inclination: | 43.0009° |
| perigee height: | 354 km |
| apogee height: | 359 km |
| right ascension of ascending node: | 55.0689° |
| argument of perigee: | 281.3604° |
| revolutions per day: | 15.70952013 |
| mean anomaly at epoch: | 78.6858° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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