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 56310U 26145.29470447 +.00000000 +00000-0 +39622-3 0 00008
2 56310 9.9894 10.8615 0000931 266.3039 93.7068 14.96403649 08
| Epoch (UTC): | 25 May 2026 07:04:22 |
| Eccentricity: | 0.0000931 |
| inclination: | 9.9894° |
| perigee height: | 577 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 10.8615° |
| argument of perigee: | 266.3039° |
| revolutions per day: | 14.96403649 |
| mean anomaly at epoch: | 93.7068° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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