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 59220U 26145.44533326 +.00000000 +00000-0 +18763-4 0 00008
2 59220 53.1600 157.9324 0001187 78.0536 282.0600 15.34387708 06
| Epoch (UTC): | 25 May 2026 10:41:16 |
| Eccentricity: | 0.0001187 |
| inclination: | 53.1600° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 157.9324° |
| argument of perigee: | 78.0536° |
| revolutions per day: | 15.34387708 |
| mean anomaly at epoch: | 282.0600° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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