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 65752U 26145.51221920 +.00000000 +00000-0 +67920-3 0 00005
2 65752 53.1617 336.1911 0002396 83.9449 276.1824 15.30222939 07
| Epoch (UTC): | 25 May 2026 12:17:35 |
| Eccentricity: | 0.0002396 |
| inclination: | 53.1617° |
| perigee height: | 474 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 336.1911° |
| argument of perigee: | 83.9449° |
| revolutions per day: | 15.30222939 |
| mean anomaly at epoch: | 276.1824° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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