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 65020U 26145.00002315 +.00000000 +00000-0 +21878-3 0 00004
2 65020 53.1584 299.5069 0000857 75.7020 36.1163 15.34391551 09
| Epoch (UTC): | 25 May 2026 00:00:02 |
| Eccentricity: | 0.0000857 |
| inclination: | 53.1584° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 299.5069° |
| argument of perigee: | 75.7020° |
| revolutions per day: | 15.34391551 |
| mean anomaly at epoch: | 36.1163° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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