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 65524U 26145.46682117 +.00000000 +00000-0 +81029-3 0 00001
2 65524 97.4514 215.1022 0002296 127.2035 232.9402 15.05673220 09
| Epoch (UTC): | 25 May 2026 11:12:13 |
| Eccentricity: | 0.0002296 |
| inclination: | 97.4514° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 215.1022° |
| argument of perigee: | 127.2035° |
| revolutions per day: | 15.05673220 |
| mean anomaly at epoch: | 232.9402° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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