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 59421U 26145.23550890 +.00000000 +00000-0 +33551-4 0 00005
2 59421 53.1585 76.6746 0001129 75.1761 284.9382 15.69714067 08
| Epoch (UTC): | 25 May 2026 05:39:07 |
| Eccentricity: | 0.0001129 |
| inclination: | 53.1585° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 76.6746° |
| argument of perigee: | 75.1761° |
| revolutions per day: | 15.69714067 |
| mean anomaly at epoch: | 284.9382° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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