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 43786U 26145.09569214 +.00000000 +00000-0 +32508-3 0 00006
2 43786 97.4047 197.0718 0014206 76.6272 283.6545 15.18708379 09
| Epoch (UTC): | 25 May 2026 02:17:47 |
| Eccentricity: | 0.0014206 |
| inclination: | 97.4047° |
| perigee height: | 500 km |
| apogee height: | 520 km |
| right ascension of ascending node: | 197.0718° |
| argument of perigee: | 76.6272° |
| revolutions per day: | 15.18708379 |
| mean anomaly at epoch: | 283.6545° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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