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 53651U 26145.66668980 +.00000000 +00000-0 +26035-2 0 00008
2 53651 97.6045 28.8482 0001944 74.8086 319.4743 15.43223863 04
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001944 |
| inclination: | 97.6045° |
| perigee height: | 435 km |
| apogee height: | 438 km |
| right ascension of ascending node: | 28.8482° |
| argument of perigee: | 74.8086° |
| revolutions per day: | 15.43223863 |
| mean anomaly at epoch: | 319.4743° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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