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 65186U 26145.40056523 +.00000000 +00000-0 +17794-3 0 00003
2 65186 97.4491 17.8945 0002476 79.9835 280.1671 15.05660769 06
| Epoch (UTC): | 25 May 2026 09:36:48 |
| Eccentricity: | 0.0002476 |
| inclination: | 97.4491° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 17.8945° |
| argument of perigee: | 79.9835° |
| revolutions per day: | 15.05660769 |
| mean anomaly at epoch: | 280.1671° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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