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 64732U 26145.38591203 +.00000000 +00000-0 +44351-3 0 00004
2 64732 53.1580 184.8494 0001018 86.9497 273.1620 15.30212273 04
| Epoch (UTC): | 25 May 2026 09:15:42 |
| Eccentricity: | 0.0001018 |
| inclination: | 53.1580° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.8494° |
| argument of perigee: | 86.9497° |
| revolutions per day: | 15.30212273 |
| mean anomaly at epoch: | 273.1620° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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