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 65153U 26145.40890564 +.00000000 +00000-0 +31028-4 0 00005
2 65153 51.8981 193.8783 0000365 85.8388 274.2616 14.79932552 02
| Epoch (UTC): | 25 May 2026 09:48:49 |
| Eccentricity: | 0.0000365 |
| inclination: | 51.8981° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 193.8783° |
| argument of perigee: | 85.8388° |
| revolutions per day: | 14.79932552 |
| mean anomaly at epoch: | 274.2616° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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