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 37792U 26106.25521524 +.00000000 +00000-0 +68141-4 0 00006
2 37792 98.2428 37.5577 0051765 200.8139 159.0965 14.80955165 03
| Epoch (UTC): | 16 April 2026 06:07:30 |
| Eccentricity: | 0.0051765 |
| inclination: | 98.2428° |
| perigee height: | 590 km |
| apogee height: | 663 km |
| right ascension of ascending node: | 37.5577° |
| argument of perigee: | 200.8139° |
| revolutions per day: | 14.80955165 |
| mean anomaly at epoch: | 159.0965° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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