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 59208U 26145.44112513 +.00000000 +00000-0 +23683-4 0 00002
2 59208 53.1598 157.9079 0001113 85.6106 274.5024 15.34395058 04
| Epoch (UTC): | 25 May 2026 10:35:13 |
| Eccentricity: | 0.0001113 |
| inclination: | 53.1598° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 157.9079° |
| argument of perigee: | 85.6106° |
| revolutions per day: | 15.34395058 |
| mean anomaly at epoch: | 274.5024° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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