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 63548U 26145.43577115 +.00000000 +00000-0 +14005-2 0 00002
2 63548 43.0015 50.7681 0001683 267.5027 92.5648 15.70887104 00
| Epoch (UTC): | 25 May 2026 10:27:30 |
| Eccentricity: | 0.0001683 |
| inclination: | 43.0015° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 50.7681° |
| argument of perigee: | 267.5027° |
| revolutions per day: | 15.70887104 |
| mean anomaly at epoch: | 92.5648° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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