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 62310U 26145.41769632 +.00000000 +00000-0 +49379-3 0 00006
2 62310 53.1593 197.3647 0001101 85.0590 275.0538 15.34403287 04
| Epoch (UTC): | 25 May 2026 10:01:28 |
| Eccentricity: | 0.0001101 |
| inclination: | 53.1593° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 197.3647° |
| argument of perigee: | 85.0590° |
| revolutions per day: | 15.34403287 |
| mean anomaly at epoch: | 275.0538° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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