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 57952U 26144.97084125 +.00000000 +00000-0 +23298-3 0 00001
2 57952 53.1593 29.8028 0001251 89.8001 270.3143 15.30208831 01
| Epoch (UTC): | 24 May 2026 23:18:00 |
| Eccentricity: | 0.0001251 |
| inclination: | 53.1593° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 29.8028° |
| argument of perigee: | 89.8001° |
| revolutions per day: | 15.30208831 |
| mean anomaly at epoch: | 270.3143° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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