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 62782U 26145.52091662 +.00000000 +00000-0 +55234-3 0 00009
2 62782 53.1595 324.9215 0001353 108.0406 252.0743 15.31729946 02
| Epoch (UTC): | 25 May 2026 12:30:07 |
| Eccentricity: | 0.0001353 |
| inclination: | 53.1595° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 324.9215° |
| argument of perigee: | 108.0406° |
| revolutions per day: | 15.31729946 |
| mean anomaly at epoch: | 252.0743° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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