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 59646U 26145.13403170 +.00000000 +00000-0 +78824-4 0 00003
2 59646 43.0022 68.0430 0001077 264.6614 95.4115 15.27586402 03
| Epoch (UTC): | 25 May 2026 03:13:00 |
| Eccentricity: | 0.0001077 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 68.0430° |
| argument of perigee: | 264.6614° |
| revolutions per day: | 15.27586402 |
| mean anomaly at epoch: | 95.4115° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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