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 62582U 26145.63896713 +.00000000 +00000-0 +75948-4 0 00004
2 62582 54.9822 10.3455 0012581 48.0187 312.1839 13.80607053 08
| Epoch (UTC): | 25 May 2026 15:20:06 |
| Eccentricity: | 0.0012581 |
| inclination: | 54.9822° |
| perigee height: | 953 km |
| apogee height: | 971 km |
| right ascension of ascending node: | 10.3455° |
| argument of perigee: | 48.0187° |
| revolutions per day: | 13.80607053 |
| mean anomaly at epoch: | 312.1839° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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