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 62319U 26145.40166821 +.00000000 +00000-0 +27579-3 0 00003
2 62319 53.1581 184.4776 0001089 87.3842 272.7283 15.30205972 08
| Epoch (UTC): | 25 May 2026 09:38:24 |
| Eccentricity: | 0.0001089 |
| inclination: | 53.1581° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.4776° |
| argument of perigee: | 87.3842° |
| revolutions per day: | 15.30205972 |
| mean anomaly at epoch: | 272.7283° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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