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 43783U 26145.08050714 +.00000000 +00000-0 +63678-4 0 00005
2 43783 97.4277 178.0612 0006372 130.4440 229.7341 14.99801738 00
| Epoch (UTC): | 25 May 2026 01:55:55 |
| Eccentricity: | 0.0006372 |
| inclination: | 97.4277° |
| perigee height: | 563 km |
| apogee height: | 572 km |
| right ascension of ascending node: | 178.0612° |
| argument of perigee: | 130.4440° |
| revolutions per day: | 14.99801738 |
| mean anomaly at epoch: | 229.7341° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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