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 53915U 26145.66668980 +.00000000 +00000-0 +19033-2 0 00001
2 53915 53.2158 307.8080 0000926 10.0116 154.5142 15.93236550 02
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0000926 |
| inclination: | 53.2158° |
| perigee height: | 293 km |
| apogee height: | 294 km |
| right ascension of ascending node: | 307.8080° |
| argument of perigee: | 10.0116° |
| revolutions per day: | 15.93236550 |
| mean anomaly at epoch: | 154.5142° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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