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 51744U 26145.52741100 +.00000000 +00000-0 +12629-3 0 00005
2 51744 53.2137 334.2105 0001313 79.7529 280.3612 15.08830985 08
| Epoch (UTC): | 25 May 2026 12:39:28 |
| Eccentricity: | 0.0001313 |
| inclination: | 53.2137° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 334.2105° |
| argument of perigee: | 79.7529° |
| revolutions per day: | 15.08830985 |
| mean anomaly at epoch: | 280.3612° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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