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 62761U 26145.47749867 +.00000000 +00000-0 +66811-3 0 00000
2 62761 53.1600 325.3652 0001390 89.3964 270.7198 15.34407820 05
| Epoch (UTC): | 25 May 2026 11:27:35 |
| Eccentricity: | 0.0001390 |
| inclination: | 53.1600° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 325.3652° |
| argument of perigee: | 89.3964° |
| revolutions per day: | 15.34407820 |
| mean anomaly at epoch: | 270.7198° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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