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 59510U 26145.64871682 +.00000000 +00000-0 +38889-3 0 00002
2 59510 97.4140 226.0029 0002308 140.9040 219.2365 15.24654371 05
| Epoch (UTC): | 25 May 2026 15:34:09 |
| Eccentricity: | 0.0002308 |
| inclination: | 97.4140° |
| perigee height: | 490 km |
| apogee height: | 493 km |
| right ascension of ascending node: | 226.0029° |
| argument of perigee: | 140.9040° |
| revolutions per day: | 15.24654371 |
| mean anomaly at epoch: | 219.2365° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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