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 51822U 26145.62648421 +.00000000 +00000-0 +64627-4 0 00001
2 51822 97.8087 153.3623 0001585 90.7359 269.4040 14.88415933 05
| Epoch (UTC): | 25 May 2026 15:02:08 |
| Eccentricity: | 0.0001585 |
| inclination: | 97.8087° |
| perigee height: | 602 km |
| apogee height: | 604 km |
| right ascension of ascending node: | 153.3623° |
| argument of perigee: | 90.7359° |
| revolutions per day: | 14.88415933 |
| mean anomaly at epoch: | 269.4040° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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