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 61510U 26145.29094466 +.00000000 +00000-0 +23902-4 0 00004
2 61510 53.1592 146.4237 0001079 85.8300 274.2825 15.31703942 03
| Epoch (UTC): | 25 May 2026 06:58:57 |
| Eccentricity: | 0.0001079 |
| inclination: | 53.1592° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 146.4237° |
| argument of perigee: | 85.8300° |
| revolutions per day: | 15.31703942 |
| mean anomaly at epoch: | 274.2825° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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