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 51444U 26145.60410963 +.00000000 +00000-0 +79177-4 0 00003
2 51444 97.8891 329.5296 0001440 88.2126 271.9252 14.82155599 01
| Epoch (UTC): | 25 May 2026 14:29:55 |
| Eccentricity: | 0.0001440 |
| inclination: | 97.8891° |
| perigee height: | 622 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 329.5296° |
| argument of perigee: | 88.2126° |
| revolutions per day: | 14.82155599 |
| mean anomaly at epoch: | 271.9252° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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