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 63752U 26145.48228272 +.00000000 +00000-0 +12937-2 0 00003
2 63752 43.0022 189.3083 0002956 259.7400 100.3134 15.70929482 06
| Epoch (UTC): | 25 May 2026 11:34:29 |
| Eccentricity: | 0.0002956 |
| inclination: | 43.0022° |
| perigee height: | 354 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 189.3083° |
| argument of perigee: | 259.7400° |
| revolutions per day: | 15.70929482 |
| mean anomaly at epoch: | 100.3134° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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